SKYBEE-A02, 64544
Orbit data source: Space-Track
SKYBEE-A02, 64544 is a payload satellite owned by ConstellR (DE) in SSO that was launched on Mon, 23 Jun 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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64544 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U MP42, Unknown motor
Mass
110 kg wet, 110 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.146 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SKYBEE-A02
1 64544U 25135S 25328.39040988 .00003976 00000-0 19527-3 0 9992
2 64544 97.4593 80.5900 0002839 118.5166 241.6354 15.18640909 23737Epoch: 2025-11-24T09:22Z
TLE epoch observation values (Epoch: 2025-11-24T09:22:11.413Z)
Latitude
-0.00007°
Longitude
-123.54861°
Altitude
513.964 km
Speed
7.606 km/s
True Right ascension
05h 22m 21s
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
16:07:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.872 km
Perigee altitude
504.962 km
Semi-major axis
6,885.054 km
Eccentricity
0.00028
Inclination
97.4593°
RAAN
80.59°
Arg. of periapsis
118.5166°
True anomaly
241.60678°
Mean anomaly
241.6354°
Eccentric anomaly
241.62109°
Mean motion
3.79911 °/min
Orbital period
94.76 mins
BSTAR
0.00019527
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-A02 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 | 2025-11-24 21:00:27.037Z | 345.396° N | 2025-11-24 21:02:27.037Z | 299.267° NW | 30.036° | 2025-11-24 21:05:27.037Z | 225.202° WSW |
| 5 mins | 2025-11-25 07:39:27.037Z | 163.165° S | 2025-11-25 07:41:27.037Z | 7.623° NNE | 43.894° | 2025-11-25 07:44:27.037Z | 349.53° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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