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5 satellites

Success

Kinetica 1

T-minus to liftoff

HOURS

MINUTES

SECONDS

Thursday July 23 2026, 23:33:00 UTC

StatusSuccess

VehicleKinetica 1

OrbitSun-Synchronous Orbit

PadLaunch Area 130

Launch CodexDossier

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General trajectory

3 hazard areas

Launch Area 130

Jiuquan Satellite Launch Center, People's Republic of China

Launching

South

190° · S

40.818, 100.225

Orbital elements (TLE)

Orbit

Apogee548 km

Perigee529 km

Period95.4 min

Inclination97.70°

Launch heading 190° · S from LJ-1 5 satellites.

OrbitLJ-1 5 satellites› conelow

1 70151U 26170A 26204.99097222 .00000000 00000-0 00000-0 0 9994

2 70151 97.7021 212.0764 0014098 278.3033 255.2164 15.09188774 07

Pre-launch TLEs from Dillon's Space Page. Estimated before flight — the real orbit is confirmed post-launch.

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Mission

Share-ride of 5 commercial Earth observation and technology demonstration satellites to SSO, including SpaceTY's Tianyi-48: * Yinglong Fengguang-1 * Zhonghang Hongwai 1/Xiguang 2-03 * Tianyi-48 (Chenguang-1) * Gande 1-01 * Jitianxing A-04

Q's read

Hazards (4)

A2002/26 NOTAMN Q) VOMF/QWLLW/IV/BO/W/000/999/ A) VOMF B) 2607010830 C) 2607291045 D) 01 08 22 29 0830-1045 15 0230-1045 23 24 1130-1715 E) GPS SONDE HIGH ALT BALLOON ASCENT FM THUMBA EQUATORIAL ROCKET LAUNCHING STN (TERLS) RANGE. LAUNCH COORD: ?083200N 0765218E DESCRIPTION: ?WHITE ORDINARY MET BALLOON WITH 2M DIAMETER INSTR WT: ?GPS SONDE 900GRAM-1800 GRAM MAX ALT EXP:?32 KM TRANSPONDER FREQ:400MHZ-405MHZ RATE OF ASCENT:?4-5 MPS RATE OF DESCENT?25 MPS (UPTO 20KM) ? ?5 MPS (BLW 20KM) EXP FLOATING TIME: 0215 HR F) GND G) UNL
E2672/26 NOTAMN Q) YMMM/QRDCA/IV/BO/W/000/999/1351S09159E170 A) YMMM B) 2607240200 C) 2607300800 D) DAILY 0200-0800 E) TEMPO DANGER AREA ACT DUE CHINESE AEROSPACE FLIGHT ACTIVITIES WILL TAKE PLACE FLW RECEIVED FM CIVIL AVIATION ADMINISTRATION OF CHINA: THE FLIGHT SAFETY OF ACFT MAY BE AFFECTED IN THE FOLLOWING 'AREA PV' BOUNDED BY: 1631S 09121E - 1110S 09205E - 1114S 09238E - 1635S 09154E - 1631S 09121E TO BEGINNING. F) SFC G) UNL
R1030/26 NOTAMN Q)RJJJ/QWPLW/IV/M/W/000/040/3621N14041E006 A)RJJJ B)2607240000 C)2607240700 E)PJE: 1.LDG SITE : BOUNDED BY FLW POINTS 362511N1403948E - 362511N1404448E - 361811N1404038E - 361811N1403538E - 362511N1403948E (AROUND HITACHINAKA-SHI,HIGASHIIBARAKI-GUN IN IBARAKI) 2.USING ACFT: H60 3.WX COND : VMC ONLY RMK:SOURCE/JSDF-A(RJAH) F)SFC G)4000FT AMSL
HYDROPAC 2081/26. INDIAN OCEAN. 1. HAZARDOUS OPERATIONS, SPACE DEBRIS 232200Z TO 240400Z JUL IN AREA BOUND BY 16-58.00S 091-51.00E, 16-54.00S 091-18.00E, 11-33.00S 092-02.00E, 11-37.00S 092-35.00E. 2. CANCEL THIS MSG 240500Z JUL 26.

Quick facts

VehicleKinetica 1

OrbitSun-Synchronous Orbit

PadLaunch Area 130

SiteJiuquan Satellite Launch Center, People's Republic of China

WindowThursday July 23 2026, 23:24:00 UTC→Thursday July 23 2026, 23:50:00 UTC

Vehicle

Height30 m

Diameter2.7 m

Stages4

ReusableNo

LEO capacity2,000 kg

Track record14/15 successful