Showing default

TJS-16, 63397

Orbit data source: Space-Track

TJS-16, 63397 is a payload satellite owned by PLA SSF (CN) in GEO that was launched on Sat, 29 Mar 2025 UTC via a CHANG ZHENG 7A launch vehicle from the Wenchang Satellite Launch Center (WSC). 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.

Not visible in the next 10 days
Identifier
63397, 2025-064A
Orbit
GEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SISE
Mission
Operational Defense Technology
Bus & Motor
FY-4?, LAE
Mass
~5,000 kg wet, ~2,500 kg dry
Launch date (UTC)
2025-03-29 (1 year ago)
Launch vehicle
CHANG ZHENG 7A
Launch site
Wenchang Satellite Launch Center (WSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 22.5 m
Radar Cross Section
34.063 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 TJS-16
1 63397U 25064A   26097.78044825 -.00000102  00000-0  00000+0 0  9990
2 63397   0.9159  81.7116 0004897 274.8179 281.0753  1.00272142  3686
Epoch: 2026-04-07T18:43Z
TLE epoch observation values (Epoch: 2026-04-07T18:43:50.728Z)
Latitude
-0.23367°
Longitude
160.53792°
Altitude
35,782.109 km
Speed
3.075 km/s
True Right ascension
18h 30m 12s
True Declination
0° 14' 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
20:32:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,808.213 km
Perigee altitude
35,766.916 km
Semi-major axis
42,165.702 km
Eccentricity
0.00049
Inclination
0.9159°
RAAN
81.7116°
Arg. of periapsis
274.8179°
True anomaly
281.02022°
Mean anomaly
281.0753°
Eccentric anomaly
281.04776°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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 #64 in the year 2025 (2025-03-29 UTC)

Documentation

Showing up to 5 results
|