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YAOGAN-40 02C, 63920

Orbit data source: Space-Track

YAOGAN-40 02C, 63920 is a payload satellite in LEO that was launched on Sun, 11 May 2025 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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.

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Identifier
63920, 2025-096C
Orbit
LEO
Last TLE update
11 hours ago
Origin
Unknown
Manufacturer
DFH
Mission
Operational spacecraft
Bus & Motor
YG40, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
2025-05-11 (2 weeks ago)
Launch vehicle
CHANG ZHENG 6A
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history

TLE from 11 hours ago
0 YAOGAN-40 02C
1 63920U 25096C   25143.93806808  .00000314  00000-0  11104-3 0  9997
2 63920  85.9952   2.4199 0013606 249.7174 170.1345 14.31337582 20375
Epoch: 2025-05-23T22:30Z
TLE epoch observation values (Epoch: 2025-05-23T22:30:49.082Z)
Latitude
59.73282°
Longitude
149.78278°
Altitude
807.099 km
Speed
7.45 km/s
True Right ascension
00h 37m 05s
True Declination
59° 35' 02"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-12.8546°
Longitude
141.79904°
Altitude
794.393 km
Speed
7.455 km/s
Apparent Right ascension
02h 43m 02s
Apparent Declination
-37° 11' 21"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:03:42
Azimuth
108.999° ESE
Elevation
-40.125°
Doppler factor
1
Orbital elements
Apogee altitude
793.986 km
Perigee altitude
774.495 km
Semi-major axis
7,162.377 km
Eccentricity
0.00136
Inclination
85.9952°
RAAN
2.4199°
Arg. of periapsis
249.7174°
True anomaly
Unknown
Mean anomaly
170.1345°
Eccentric anomaly
Unknown
Mean motion
3.58061 °/min
Orbital period
100.54 mins
BSTAR
0.00011104
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Other satellites on launch #96 in the year 2025 (2025-05-11 UTC)

YAOGAN-40 02C Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
10 mins2025-05-24 15:07:10.033Z181.107° SSW2025-05-24 15:12:10.033Z8.042° NNE44.766°2025-05-24 15:17:10.033Z3.262° NNE
6 mins2025-05-25 01:41:10.033Z40.352° NE2025-05-25 01:43:10.033Z70.901° E22.804°2025-05-25 01:47:10.033Z127.894° SE
8 mins2025-05-25 03:21:10.033Z331.128° NNW2025-05-25 03:24:10.033Z284.887° WNW29.937°2025-05-25 03:29:10.033Z210.617° SW
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