OBJECT G, 60241
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 G, 60241 is a satellite in LEO that was launched on Tue, 09 Jul 2024 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). 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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60241 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
ORBMAT
Mission
Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT G
1 60241U 24128G 25261.08922351 .00004744 00000-0 34435-3 0 9997
2 60241 61.9902 88.0610 0056524 79.4594 281.2859 15.04072030 65339Epoch: 2025-09-18T02:08Z
TLE epoch observation values (Epoch: 2025-09-18T02:08:28.911Z)
Latitude
0.00002°
Longitude
58.68472°
Altitude
548.671 km
Speed
7.592 km/s
True Right ascension
05h 52m 14s
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
05:27:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.464 km
Perigee altitude
514.106 km
Semi-major axis
6,931.422 km
Eccentricity
0.00565
Inclination
61.9902°
RAAN
88.061°
Arg. of periapsis
79.4594°
True anomaly
280.64984°
Mean anomaly
281.2859°
Eccentric anomaly
280.96796°
Mean motion
3.76105 °/min
Orbital period
95.72 mins
BSTAR
0.00034435
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Other satellites on launch #128 in the year 2024 (2024-07-09 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 G 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 15:05:33.503Z | 249.681° W | 2025-09-18 15:07:33.503Z | 312.985° NW | 35.404° | 2025-09-18 15:10:33.503Z | 20.724° NNE |
| 4 mins | 2025-09-18 21:48:33.503Z | 15.083° NNE | 2025-09-18 21:49:33.503Z | 34.057° NE | 17.779° | 2025-09-18 21:52:33.503Z | 85.84° E |
| 6 mins | 2025-09-18 23:26:33.503Z | 303.019° NW | 2025-09-18 23:28:33.503Z | 255.361° W | 35.045° | 2025-09-18 23:32:33.503Z | 166.24° S |
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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