OOV-CUBE, 60240
Orbit data source: Space-Track
OOV-CUBE, 60240 is a payload satellite owned by TUB (DE) in LEO that was launched on Tue, 09 Jul 2024 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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60240 intel report (Beta)
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OOV-CUBE radio frequencies
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
TUB
Mission
Operational Amateur Technology
Bus & Motor
TUBSAT, Unknown motor
Mass
17 kg wet, 17 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.094 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OOV-CUBE
1 60240U 24128F 25260.95591744 .00002794 00000-0 22761-3 0 9991
2 60240 61.9944 93.5932 0058014 76.3708 284.3834 15.00806726 65229Epoch: 2025-09-17T22:56Z
TLE epoch observation values (Epoch: 2025-09-17T22:56:31.266Z)
Latitude
-0.00001°
Longitude
112.33848°
Altitude
556.391 km
Speed
7.589 km/s
True Right ascension
06h 14m 22s
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
01:35:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.608 km
Perigee altitude
523.068 km
Semi-major axis
6,941.475 km
Eccentricity
0.0058
Inclination
61.9944°
RAAN
93.5932°
Arg. of periapsis
76.3708°
True anomaly
283.7383°
Mean anomaly
284.3834°
Eccentric anomaly
284.06096°
Mean motion
3.75289 °/min
Orbital period
95.93 mins
BSTAR
0.00022761
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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.OOV-CUBE 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 | 2025-09-18 15:04:50.037Z | 221.731° SW | 2025-09-18 15:08:50.037Z | 349.479° N | 42.751° | 2025-09-18 15:11:50.037Z | 31.304° NE |
| 4 mins | 2025-09-18 21:49:50.037Z | 9.059° NNE | 2025-09-18 21:51:50.037Z | 40.932° NE | 13.819° | 2025-09-18 21:53:50.037Z | 71.259° E |
| 6 mins | 2025-09-18 23:28:50.037Z | 316.901° NNW | 2025-09-18 23:30:50.037Z | 272.601° WNW | 43.256° | 2025-09-18 23:34:50.037Z | 151.906° SSE |
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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