INNOCUBE (TUSAT-31), 62616
Orbit data source: Space-Track
INNOCUBE (TUSAT-31), 62616 is a payload satellite owned by TUB (DE) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62616 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
TUB
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~4 kg wet, ~4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 INNOCUBE (TUSAT-31)
1 62616U 25009H 25286.26465871 .00012863 00000-0 57055-3 0 9994
2 62616 97.4136 4.3404 0007865 118.1970 242.0061 15.21692895 41201Epoch: 2025-10-13T06:21Z
TLE epoch observation values (Epoch: 2025-10-13T06:21:06.512Z)
Latitude
-0.00005°
Longitude
-113.00666°
Altitude
506.37 km
Speed
7.61 km/s
True Right ascension
00h 17m 21s
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
08:57:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.106 km
Perigee altitude
492.29 km
Semi-major axis
6,875.835 km
Eccentricity
0.00079
Inclination
97.4136°
RAAN
4.3404°
Arg. of periapsis
118.197°
True anomaly
241.92656°
Mean anomaly
242.0061°
Eccentric anomaly
241.96632°
Mean motion
3.80676 °/min
Orbital period
94.57 mins
BSTAR
0.00057055
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.INNOCUBE (TUSAT-31) 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 | 2025-10-13 17:57:23.417Z | 20.933° NNE | 2025-10-13 18:00:23.417Z | 71.395° E | 38.902° | 2025-10-13 18:03:23.417Z | 176.371° S |
| 4 mins | 2025-10-14 04:36:23.417Z | 105.803° ESE | 2025-10-14 04:38:23.417Z | 60.59° ENE | 20.281° | 2025-10-14 04:40:23.417Z | 23.469° NE |
| 4 mins | 2025-10-14 06:10:23.417Z | 235.688° WSW | 2025-10-14 06:11:23.417Z | 257.642° W | 19.687° | 2025-10-14 06:14:23.417Z | 314.723° NW |
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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