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 (1 month ago)
Launch vehicle
CHANG ZHENG 2F
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 PRC TEST SPACECRAFT 4
1 67689U 26024A   26071.97676774  .00000178  00000-0  41509-4 0  9998
2 67689  49.9871   7.3415 0006028  13.2035 346.9064 14.91691119  5072
Epoch: 2026-03-12T23:26Z
TLE epoch observation values (Epoch: 2026-03-12T23:26:32.732Z)
Latitude
0.00002°
Longitude
-154.91379°
Altitude
589.114 km
Speed
7.569 km/s
True Right ascension
00h 29m 21s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
12:16:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.628 km
Perigee altitude
589.223 km
Semi-major axis
6,971.562 km
Eccentricity
0.0006
Inclination
49.9871°
RAAN
7.3415°
Arg. of periapsis
13.2035°
True anomaly
346.89074°
Mean anomaly
346.9064°
Eccentric anomaly
346.89857°
Mean motion
3.72862 °/min
Orbital period
96.55 mins
BSTAR
0.000041509
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...
Other satellites on launch #24 in the year 2026 (2026-02-07 UTC)

Documentation

Showing up to 5 results
|