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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 SKYBEE-A02
1 64544U 25135S 26120.20902845 .00003136 00000-0 14950-3 0 9995
2 64544 97.4674 235.5147 0001320 17.9103 342.2178 15.19842912 47545Epoch: 2026-04-30T05:01Z
TLE epoch observation values (Epoch: 2026-04-30T05:01:00.058Z)
Latitude
-0.00001°
Longitude
-57.89446°
Altitude
508.538 km
Speed
7.61 km/s
True Right ascension
15h 42m 03s
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
16:38:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.192 km
Perigee altitude
502.375 km
Semi-major axis
6,881.421 km
Eccentricity
0.00013
Inclination
97.4674°
RAAN
235.5147°
Arg. of periapsis
17.9103°
True anomaly
342.21318°
Mean anomaly
342.2178°
Eccentric anomaly
342.21549°
Mean motion
3.80212 °/min
Orbital period
94.68 mins
BSTAR
0.0001495
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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 | 2026-04-30 19:48:42.322Z | 44.316° NE | 2026-04-30 19:51:42.322Z | 104.719° ESE | 21.532° | 2026-04-30 19:53:42.322Z | 143.406° SSE |
| 4 mins | 2026-04-30 21:23:42.322Z | 320.559° NNW | 2026-04-30 21:24:42.322Z | 299.83° NW | 19.01° | 2026-04-30 21:27:42.322Z | 243.482° WSW |
| 6 mins | 2026-05-01 07:59:42.322Z | 184.473° SSW | 2026-05-01 08:02:42.322Z | 235.555° WSW | 36.119° | 2026-05-01 08:05:42.322Z | 331.52° NNW |
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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