OBJECT E, 61242
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 E, 61242 is a Chinese satellite in SSO that was launched on Tue, 24 Sep 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.
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61242 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
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 & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 OBJECT E
1 61242U 24174E 25321.86896708 .00008921 00000-0 36711-3 0 9999
2 61242 97.4517 328.5557 0012149 258.2163 101.7712 15.24303017 63610Epoch: 2025-11-17T20:51Z
TLE epoch observation values (Epoch: 2025-11-17T20:51:18.755Z)
Latitude
-0.00001°
Longitude
-41.43567°
Altitude
497.687 km
Speed
7.615 km/s
True Right ascension
21h 54m 13s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:09:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.185 km
Perigee altitude
481.497 km
Semi-major axis
6,867.978 km
Eccentricity
0.00121
Inclination
97.4517°
RAAN
328.5557°
Arg. of periapsis
258.2163°
True anomaly
101.90745°
Mean anomaly
101.7712°
Eccentric anomaly
101.83933°
Mean motion
3.81329 °/min
Orbital period
94.41 mins
BSTAR
0.00036711
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Other satellites on launch #174 in the year 2024 (2024-09-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT E Visibility forecast
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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 mins | 2025-11-18 13:10:10.880Z | 23.751° NE | 2025-11-18 13:13:10.880Z | 80.071° E | 36.887° | 2025-11-18 13:16:10.880Z | 172.346° S |
| 4 mins | 2025-11-18 23:48:10.880Z | 99.351° ESE | 2025-11-18 23:49:10.880Z | 79.292° E | 18.12° | 2025-11-18 23:52:10.880Z | 23.217° NE |
| 4 mins | 2025-11-19 01:21:10.880Z | 221.583° SW | 2025-11-19 01:23:10.880Z | 267.15° W | 22.342° | 2025-11-19 01:25:10.880Z | 309.832° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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