DECAYED

OBJECT F, 61263 (Decayed)

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 F, 61263 was a satellite owned by CASC (CN) in LEO that was launched on Tue, 24 Sep 2024 UTC launched 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. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
61263, 2024-174F
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
CAS
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
500 kg wet, 500 kg dry
Launch date (UTC)
2024-09-24 (1 year ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
8.585 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 OBJECT F
1 61263U 24174F   24361.00147284  .15275069  25412-5  27479-3 0  9994
2 61263  97.4017  12.9117 0012552  63.2520 327.2527 16.46835838 14456
Epoch: 2024-12-26T00:02Z
TLE epoch observation values (Epoch: 2024-12-26T00:02:07.253Z)
Latitude
30.20471°
Longitude
-86.91754°
Altitude
144.843 km
Speed
7.826 km/s
True Right ascension
00h 34m 23s
True Declination
30° 02' 29"
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
15:24:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
152.667 km
Perigee altitude
136.293 km
Semi-major axis
6,522.617 km
Eccentricity
0.00126
Inclination
97.4017°
RAAN
12.9117°
Arg. of periapsis
63.252°
True anomaly
327.17479°
Mean anomaly
327.2527°
Eccentric anomaly
327.21376°
Mean motion
4.12012 °/min
Orbital period
87.38 mins
BSTAR
0.00027479
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
|