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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SKYBEE-A02
1 64544U 25135S 26171.42673274 .00002057 00000-0 98388-4 0 9995
2 64544 97.4738 286.2295 0003131 118.7618 241.3932 15.20112779 55321Epoch: 2026-06-20T10:14Z
TLE epoch observation values (Epoch: 2026-06-20T10:14:29.708Z)
Latitude
-0.00002°
Longitude
-136.0358°
Altitude
509.621 km
Speed
7.609 km/s
True Right ascension
19h 04m 55s
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
07:20:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.623 km
Perigee altitude
500.314 km
Semi-major axis
6,880.606 km
Eccentricity
0.00031
Inclination
97.4738°
RAAN
286.2295°
Arg. of periapsis
118.7618°
True anomaly
241.36171°
Mean anomaly
241.3932°
Eccentric anomaly
241.37745°
Mean motion
3.8028 °/min
Orbital period
94.67 mins
BSTAR
0.000098388
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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 | 2026-06-21 06:55:26.892Z | 118.003° SE | 2026-06-21 06:58:26.892Z | 59.513° ENE | 19.949° | 2026-06-21 07:00:26.892Z | 23.356° NE |
| 4 mins | 2026-06-21 08:30:26.892Z | 234.283° WSW | 2026-06-21 08:31:26.892Z | 256.392° W | 20.312° | 2026-06-21 08:34:26.892Z | 314.673° NW |
| 4 mins | 2026-06-21 20:00:26.892Z | 52.199° ENE | 2026-06-21 20:02:26.892Z | 108.504° ESE | 26.718° | 2026-06-21 20:04:26.892Z | 151.986° SSE |
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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