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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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, 0.2 m
Radar Cross Section
0.094 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 OOV-CUBE
1 60240U 24128F 26265.52362158 .00001200 00000-0 10324-3 0 9998
2 60240 61.9930 246.0719 0030806 156.5096 203.7411 15.03116087120744Epoch: 2026-09-22T12:34Z
TLE epoch observation values (Epoch: 2026-09-22T12:34:00.904Z)
Latitude
0.00003°
Longitude
56.18028°
Altitude
578.635 km
Speed
7.561 km/s
True Right ascension
16h 24m 17s
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
22:41:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.586 km
Perigee altitude
534.862 km
Semi-major axis
6,934.361 km
Eccentricity
0.00308
Inclination
61.993°
RAAN
246.0719°
Arg. of periapsis
156.5096°
True anomaly
203.59948°
Mean anomaly
203.7411°
Eccentric anomaly
203.67024°
Mean motion
3.75866 °/min
Orbital period
95.78 mins
BSTAR
0.00010324
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-23 08:13:47.639Z | 349.992° N | 2026-09-23 08:16:47.639Z | 39.653° NE | 23.619° | 2026-09-23 08:19:47.639Z | 94.157° ESE |
| 5 mins | 2026-09-23 09:53:47.639Z | 292.633° NW | 2026-09-23 09:55:47.639Z | 243.112° WSW | 35.09° | 2026-09-23 09:58:47.639Z | 179.653° S |
| 5 mins | 2026-09-23 23:50:47.639Z | 161.45° S | 2026-09-23 23:52:47.639Z | 114.221° SE | 30.544° | 2026-09-23 23:55:47.639Z | 60.308° ENE |
| 5 mins | 2026-09-24 01:29:47.639Z | 276.271° WNW | 2026-09-24 01:31:47.639Z | 323.152° NNW | 27.856° | 2026-09-24 01:34:47.639Z | 12.861° NNE |
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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