Showing default

PRC TEST SPACECRAFT 4, 67689

Orbit data source: Space-Track

PRC TEST SPACECRAFT 4, 67689 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Sat, 07 Feb 2026 UTC via a CHANG ZHENG 2F launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
67689, 2026-024A
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CAST
Mission
Operational spacecraft
Bus & Motor
CSSHQ, Unknown motor
Mass
~8,000 kg wet, 8,000 kg dry
Launch date (UTC)
2026-02-07 (2 months ago)
Launch vehicle
CHANG ZHENG 2F
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 PRC TEST SPACECRAFT 4
1 67689U 26024A   26103.79649564  .00000004  00000-0  24388-4 0  9995
2 67689  49.9853 217.9677 0005945 139.5013 220.6372 14.91717970  9827
Epoch: 2026-04-13T19:06Z
TLE epoch observation values (Epoch: 2026-04-13T19:06:57.223Z)
Latitude
Longitude
89.24732°
Altitude
596.269 km
Speed
7.561 km/s
True Right ascension
14h 31m 52s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:12:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.486 km
Perigee altitude
589.197 km
Semi-major axis
6,971.479 km
Eccentricity
0.00059
Inclination
49.9853°
RAAN
217.9677°
Arg. of periapsis
139.5013°
True anomaly
220.59286°
Mean anomaly
220.6372°
Eccentric anomaly
220.61503°
Mean motion
3.72869 °/min
Orbital period
96.55 mins
BSTAR
0.000024388
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|