MANDRAKE 2 BAKER, 48908
Orbit data source: Space-Track
MANDRAKE 2 BAKER, 48908 is an American payload satellite in SSO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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48908 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Astro Digital
Mission
Operational Defense Communications
Bus & Motor
CORVUS-XL, Unknown motor
Mass
23 kg wet, 23 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.5 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 MANDRAKE 2 BAKER
1 48908U 21059AF 26312.31876225 .00059517 00000-0 54584-3 0 9990
2 48908 97.6843 157.7550 0003445 141.5127 218.6379 15.67568315299817Epoch: 2026-11-08T07:39Z
TLE epoch observation values (Epoch: 2026-11-08T07:39:01.058Z)
Latitude
-0.00003°
Longitude
-4.51078°
Altitude
370.824 km
Speed
7.686 km/s
True Right ascension
10h 31m 01s
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
17:47:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
365.1 km
Perigee altitude
360.455 km
Semi-major axis
6,740.915 km
Eccentricity
0.00034
Inclination
97.6843°
RAAN
157.755°
Arg. of periapsis
141.5127°
True anomaly
218.61326°
Mean anomaly
218.6379°
Eccentric anomaly
218.62558°
Mean motion
3.92161 °/min
Orbital period
91.8 mins
BSTAR
0.00054584
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Other satellites on launch #59 in the year 2021 (2021-06-30 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.MANDRAKE 2 BAKER 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 | 2026-11-09 02:35:02.905Z | 20.305° NNE | 2026-11-09 02:38:02.905Z | 129.228° SE | 55.85° | 2026-11-09 02:40:02.905Z | 179.869° S |
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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