OBJECT H, 60242
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, 60242 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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60242 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
Planetary Transportation Systems GmbH (DE)Manufacturer
PTS
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
24 kg wet, 24 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 OBJECT H
1 60242U 24128H 25315.30935563 .00015421 00000-0 97135-3 0 9992
2 60242 61.9796 255.0619 0056827 86.8386 273.9207 15.08036127 73541Epoch: 2025-11-11T07:25Z
TLE epoch observation values (Epoch: 2025-11-11T07:25:28.326Z)
Latitude
-0.00005°
Longitude
92.99609°
Altitude
541.509 km
Speed
7.594 km/s
True Right ascension
17h 00m 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
20:41:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.451 km
Perigee altitude
501.811 km
Semi-major axis
6,919.268 km
Eccentricity
0.00568
Inclination
61.9796°
RAAN
255.0619°
Arg. of periapsis
86.8386°
True anomaly
273.27073°
Mean anomaly
273.9207°
Eccentric anomaly
273.59575°
Mean motion
3.77097 °/min
Orbital period
95.47 mins
BSTAR
0.00097135
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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 H 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-12 06:12:59.448Z | 332.096° NNW | 2025-11-12 06:16:59.448Z | 73.024° E | 39.223° | 2025-11-12 06:19:59.448Z | 129.368° SE |
| 5 mins | 2025-11-12 21:46:59.448Z | 208.033° SW | 2025-11-12 21:48:59.448Z | 151.379° SSE | 44.317° | 2025-11-12 21:51:59.448Z | 39.392° NE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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