SKYBEE-A01, 62671
Orbit data source: Space-Track
SKYBEE-A01, 62671 is a payload satellite owned by ConstellR (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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62671 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U MP16, Unknown motor
Mass
110 kg wet, 110 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.3 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SKYBEE-A01
1 62671U 25009BQ 26215.90967430 .00002202 00000-0 10173-3 0 9993
2 62671 97.3965 293.6506 0006021 150.8785 209.2788 15.21219078143591Epoch: 2026-08-03T21:49Z
TLE epoch observation values (Epoch: 2026-08-03T21:49:55.859Z)
Latitude
0.00001°
Longitude
13.68184°
Altitude
508.869 km
Speed
7.608 km/s
True Right ascension
19h 34m 36s
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
20:49:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.267 km
Perigee altitude
494.985 km
Semi-major axis
6,877.263 km
Eccentricity
0.0006
Inclination
97.3965°
RAAN
293.6506°
Arg. of periapsis
150.8785°
True anomaly
209.24508°
Mean anomaly
209.2788°
Eccentric anomaly
209.26194°
Mean motion
3.80557 °/min
Orbital period
94.6 mins
BSTAR
0.00010173
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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.SKYBEE-A01 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 18:36:13.534Z | 345.223° N | 2026-08-05 18:38:13.534Z | 297.134° NW | 30.278° | 2026-08-05 18:41:13.534Z | 223.914° SW |
| 6 mins | 2026-08-06 05:13:13.534Z | 161.668° S | 2026-08-06 05:16:13.534Z | 14.317° NNE | 42.527° | 2026-08-06 05:19:13.534Z | 350.99° N |
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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