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: 17 hours ago
TLE from 17 hours ago
0 SKYBEE-A02
1 64544U 25135S 25269.20881445 .00006619 00000-0 32895-3 0 9997
2 64544 97.4540 22.2488 0001843 35.5894 324.5463 15.17979293 14757Epoch: 2025-09-26T05:00Z
TLE epoch observation values (Epoch: 2025-09-26T05:00:41.568Z)
Latitude
0.00002°
Longitude
-58.18328°
Altitude
514 km
Speed
7.607 km/s
True Right ascension
01h 28m 59s
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
15:06:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.188 km
Perigee altitude
507.65 km
Semi-major axis
6,887.056 km
Eccentricity
0.00018
Inclination
97.454°
RAAN
22.2488°
Arg. of periapsis
35.5894°
True anomaly
324.53405°
Mean anomaly
324.5463°
Eccentric anomaly
324.54017°
Mean motion
3.79746 °/min
Orbital period
94.8 mins
BSTAR
0.00032895
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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 | 2025-09-27 08:02:21.447Z | 194.047° SSW | 2025-09-27 08:04:21.447Z | 239.366° WSW | 34.346° | 2025-09-27 08:07:21.447Z | 329.043° NNW |
| 4 mins | 2025-09-27 21:08:21.447Z | 332.039° NNW | 2025-09-27 21:10:21.447Z | 278.821° WNW | 25.911° | 2025-09-27 21:12:21.447Z | 236.205° WSW |
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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