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: 1 day ago
TLE from 1 day ago
0 INNOCUBE (TUBSAT-31)
1 62616U 25009H 26170.77441444 .00005519 00000-0 21398-3 0 9994
2 62616 97.3900 250.7390 0004823 336.2696 23.8320 15.26531812 79210Epoch: 2026-06-19T18:35Z
TLE epoch observation values (Epoch: 2026-06-19T18:35:09.407Z)
Latitude
0.00001°
Longitude
63.95124°
Altitude
486.26 km
Speed
7.624 km/s
True Right ascension
16h 42m 57s
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
07:23:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.455 km
Perigee altitude
479.837 km
Semi-major axis
6,861.283 km
Eccentricity
0.00048
Inclination
97.39°
RAAN
250.739°
Arg. of periapsis
336.2696°
True anomaly
23.85434°
Mean anomaly
23.832°
Eccentric anomaly
23.84317°
Mean motion
3.81887 °/min
Orbital period
94.27 mins
BSTAR
0.00021398
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 05:19:45.978Z | 161.918° S | 2026-06-21 05:22:45.978Z | 13.601° NNE | 42.429° | 2026-06-21 05:25:45.978Z | 350.892° N |
| 5 mins | 2026-06-21 18:21:45.978Z | 1.448° NNE | 2026-06-21 18:23:45.978Z | 238.417° WSW | 42.16° | 2026-06-21 18:26:45.978Z | 199.914° SSW |
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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