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: 9 hours ago
TLE from 9 hours ago
0 OBJECT E
1 61242U 24174E 25352.65141919 .00005677 00000-0 23080-3 0 9997
2 61242 97.4504 359.1661 0014885 144.5581 215.6649 15.24842463 68300Epoch: 2025-12-18T15:38Z
TLE epoch observation values (Epoch: 2025-12-18T15:38:02.618Z)
Latitude
0.00003°
Longitude
37.15132°
Altitude
502.668 km
Speed
7.608 km/s
True Right ascension
23h 56m 39s
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
23:08:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.44 km
Perigee altitude
477.999 km
Semi-major axis
6,866.357 km
Eccentricity
0.00149
Inclination
97.4504°
RAAN
359.1661°
Arg. of periapsis
144.5581°
True anomaly
215.5656°
Mean anomaly
215.6649°
Eccentric anomaly
215.61524°
Mean motion
3.81464 °/min
Orbital period
94.37 mins
BSTAR
0.0002308
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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 | 2025-12-19 01:12:23.661Z | 201.517° SSW | 2025-12-19 01:15:23.661Z | 265.892° W | 27.127° | 2025-12-19 01:18:23.661Z | 325.458° NNW |
| 4 mins | 2025-12-19 14:15:23.661Z | 325.982° NNW | 2025-12-19 14:17:23.661Z | 278.718° WNW | 20.391° | 2025-12-19 14:19:23.661Z | 241.438° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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