INNOCUBE (TUBSAT-31), 62616
Orbit data source: Space-Track
INNOCUBE (TUBSAT-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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 INNOCUBE (TUBSAT-31)
1 62616U 25009H 26215.47096921 .00007614 00000-0 28882-3 0 9990
2 62616 97.3882 294.9822 0006608 152.5122 207.6468 15.27123528 86030Epoch: 2026-08-03T11:18Z
TLE epoch observation values (Epoch: 2026-08-03T11:18:11.739Z)
Latitude
-0.00001°
Longitude
173.37968°
Altitude
491.535 km
Speed
7.617 km/s
True Right ascension
19h 39m 55s
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
17:49:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.905 km
Perigee altitude
476.839 km
Semi-major axis
6,859.509 km
Eccentricity
0.00066
Inclination
97.3882°
RAAN
294.9822°
Arg. of periapsis
152.5122°
True anomaly
207.61169°
Mean anomaly
207.6468°
Eccentric anomaly
207.62924°
Mean motion
3.82035 °/min
Orbital period
94.23 mins
BSTAR
0.00028882
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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 (TUBSAT-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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-05 05:53:48.127Z | 203.684° SW | 2026-08-05 05:55:48.127Z | 251.631° W | 29.453° | 2026-08-05 05:58:48.127Z | 325.352° NNW |
| 4 mins | 2026-08-05 18:54:48.127Z | 332.671° NNW | 2026-08-05 18:56:48.127Z | 283.961° WNW | 23.311° | 2026-08-05 18:58:48.127Z | 240.319° WSW |
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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