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 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: 8 hours ago
TLE from 8 hours ago
0 SKYBEE-A02
1 64544U 25135S 26062.59378231 .00004971 00000-0 23775-3 0 9991
2 64544 97.4604 178.5441 0002824 130.8606 229.2874 15.19445106 38792Epoch: 2026-03-03T14:15Z
TLE epoch observation values (Epoch: 2026-03-03T14:15:02.791Z)
Latitude
-0.00001°
Longitude
163.41186°
Altitude
511.873 km
Speed
7.607 km/s
True Right ascension
11h 54m 10s
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
02:02:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.429 km
Perigee altitude
502.542 km
Semi-major axis
6,882.622 km
Eccentricity
0.00028
Inclination
97.4604°
RAAN
178.5441°
Arg. of periapsis
130.8606°
True anomaly
229.26288°
Mean anomaly
229.2874°
Eccentric anomaly
229.27514°
Mean motion
3.80113 °/min
Orbital period
94.71 mins
BSTAR
0.00023775
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-04 07:45:53.400Z | 172.322° S | 2026-03-04 07:48:53.400Z | 291.687° WNW | 44.126° | 2026-03-04 07:51:53.400Z | 344.597° N |
| 6 mins | 2026-03-04 20:50:53.400Z | 354.68° N | 2026-03-04 20:52:53.400Z | 312.411° NW | 35.436° | 2026-03-04 20:56:53.400Z | 210.701° SW |
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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