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: 12 hours ago
TLE from 12 hours ago
0 SKYBEE-A01
1 62671U 25009BQ 26253.27045726 .00001791 00000-0 83004-4 0 9996
2 62671 97.3932 330.3423 0006357 48.5185 311.6596 15.21355049149276Epoch: 2026-09-10T06:29Z
TLE epoch observation values (Epoch: 2026-09-10T06:29:27.507Z)
Latitude
0.00002°
Longitude
-116.33289°
Altitude
501.939 km
Speed
7.615 km/s
True Right ascension
22h 01m 22s
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
10:34:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.087 km
Perigee altitude
494.344 km
Semi-major axis
6,876.853 km
Eccentricity
0.00064
Inclination
97.3932°
RAAN
330.3423°
Arg. of periapsis
48.5185°
True anomaly
311.60515°
Mean anomaly
311.6596°
Eccentric anomaly
311.63238°
Mean motion
3.80591 °/min
Orbital period
94.59 mins
BSTAR
0.000083004
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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 | 2026-09-11 04:43:47.211Z | 130.412° SE | 2026-09-11 04:46:47.211Z | 59.407° ENE | 30.89° | 2026-09-11 04:48:47.211Z | 16.713° NNE |
| 5 mins | 2026-09-11 17:47:47.211Z | 32.03° NE | 2026-09-11 17:49:47.211Z | 84.922° E | 47.212° | 2026-09-11 17:52:47.211Z | 170.793° S |
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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