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: 11 hours ago
TLE from 11 hours ago
0 SKYBEE-A01
1 62671U 25009BQ 26171.37450865 .00001844 00000-0 86206-4 0 9996
2 62671 97.3990 249.9013 0004404 339.3790 20.7267 15.21019965136828Epoch: 2026-06-20T08:59Z
TLE epoch observation values (Epoch: 2026-06-20T08:59:17.547Z)
Latitude
-0.00005°
Longitude
-153.51185°
Altitude
503.02 km
Speed
7.614 km/s
True Right ascension
16h 39m 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
07:21:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.756 km
Perigee altitude
496.698 km
Semi-major axis
6,877.864 km
Eccentricity
0.00044
Inclination
97.399°
RAAN
249.9013°
Arg. of periapsis
339.379°
True anomaly
20.74457°
Mean anomaly
20.7267°
Eccentric anomaly
20.73563°
Mean motion
3.80507 °/min
Orbital period
94.61 mins
BSTAR
0.000086206
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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 | 2026-06-21 05:38:58.787Z | 194.655° SSW | 2026-06-21 05:40:58.787Z | 248.007° W | 35.52° | 2026-06-21 05:43:58.787Z | 331.361° NNW |
| 5 mins | 2026-06-21 18:42:58.787Z | 337.875° N | 2026-06-21 18:44:58.787Z | 287.696° WNW | 27.214° | 2026-06-21 18:47:58.787Z | 227.171° WSW |
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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