OBJECT H, 61901

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 H, 61901 is a satellite owned by Yunyao yuhang (CN) in SSO that was launched on Mon, 11 Nov 2024 UTC via a LIJIAN-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
61901, 2024-205H
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Changguang WJ
Mission
Operational Commercial Weather
Bus & Motor
YY-1, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2024-11-11 (10 months ago)
Launch vehicle
LIJIAN-1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)

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

TLE from 9 hours ago
0 OBJECT H
1 61901U 24205H   25256.27972523  .00007876  00000-0  33658-3 0  9993
2 61901  97.4399 330.4809 0010174 298.9550  61.0666 15.23086037 46446
Epoch: 2025-09-13T06:42Z
TLE epoch observation values (Epoch: 2025-09-13T06:42:48.259Z)
Latitude
-0.00006°
Longitude
-122.73553°
Altitude
496.253 km
Speed
7.618 km/s
True Right ascension
22h 01m 55s
True Declination
0° 00' 00"
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
08:43:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.493 km
Perigee altitude
486.511 km
Semi-major axis
6,871.639 km
Eccentricity
0.00102
Inclination
97.4399°
RAAN
330.4809°
Arg. of periapsis
298.955°
True anomaly
61.1687°
Mean anomaly
61.0666°
Eccentric anomaly
61.11764°
Mean motion
3.81024 °/min
Orbital period
94.48 mins
BSTAR
0.00033658
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
|