OBJECT A, 62729

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT A, 62729 is a satellite owned by Yunyao yuhang (CN) in SSO that was launched on Mon, 20 Jan 2025 UTC via a GUSHENXING 1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.

Loading next visibility...
Identifier
62729, 2025-013A
Orbit
SSO
Last TLE update
7 hours ago
Origin
Flag of CNYYAO (CN / PRC)
Manufacturer
Changguang WJ
Mission
Operational Commercial Weather
Bus & Motor
YY-1, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2025-01-20 (6 months ago)
Launch vehicle
GUSHENXING 1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Box + 1 Pan, 5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 7 hours ago
0 OBJECT A
1 62729U 25013A   25196.58682137  .00009693  00000-0  49737-3 0  9990
2 62729  97.6262   3.6293 0013286  40.8992 319.3235 15.16667368 26659
Epoch: 2025-07-15T14:05Z
TLE epoch observation values (Epoch: 2025-07-15T14:05:01.366Z)
Latitude
-0.00001°
Longitude
-141.30559°
Altitude
512.058 km
Speed
7.612 km/s
True Right ascension
00h 14m 31s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-80.90792°
Longitude
-17.30541°
Altitude
550.569 km
Speed
7.582 km/s
Apparent Right ascension
22h 37m 29s
Apparent Declination
-70° 09' 18"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
10:10:24
Azimuth
184.532° SSW
Elevation
-59.555°
Doppler factor
1
Orbital elements
Apogee altitude
522.056 km
Perigee altitude
503.746 km
Semi-major axis
6,891.038 km
Eccentricity
0.00133
Inclination
97.6262°
RAAN
3.6293°
Arg. of periapsis
40.8992°
True anomaly
Unknown
Mean anomaly
319.3235°
Eccentric anomaly
Unknown
Mean motion
3.79416 °/min
Orbital period
94.88 mins
BSTAR
0.00049737
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
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 #13 in the year 2025 (2025-01-20 UTC)

OBJECT A 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.
6 mins2025-07-16 00:08:55.689Z7.513° NNE2025-07-16 00:11:55.689Z250.631° W43.742°2025-07-16 00:14:55.689Z199.205° SSW
5 mins2025-07-16 10:48:55.689Z133.795° SE2025-07-16 10:50:55.689Z75.643° E33.947°2025-07-16 10:53:55.689Z5.038° NNE
|