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: 1 day ago
TLE from 1 day ago
0 MANDRAKE 2 BAKER
1 48908U 21059AF 26140.30964727 .00020365 00000-0 27259-3 0 9991
2 48908 97.7017 330.6776 0004879 95.5596 264.6216 15.58037691272958Epoch: 2026-05-20T07:25Z
TLE epoch observation values (Epoch: 2026-05-20T07:25:53.524Z)
Latitude
0.00006°
Longitude
-18.76647°
Altitude
396.781 km
Speed
7.672 km/s
True Right ascension
22h 02m 42s
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
16:20:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
393.568 km
Perigee altitude
386.963 km
Semi-major axis
6,768.402 km
Eccentricity
0.00049
Inclination
97.7017°
RAAN
330.6776°
Arg. of periapsis
95.5596°
True anomaly
264.56594°
Mean anomaly
264.6216°
Eccentric anomaly
264.59377°
Mean motion
3.89775 °/min
Orbital period
92.36 mins
BSTAR
0.00027259
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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 | 2026-05-21 12:50:59.060Z | 176.706° S | 2026-05-21 12:52:59.060Z | 215.02° SW | 40.715° | 2026-05-21 12:55:59.060Z | 341.201° N |
| 4 mins | 2026-05-22 01:36:59.060Z | 11.337° NNE | 2026-05-22 01:38:59.060Z | 201.783° SSW | 43.678° | 2026-05-22 01:40:59.060Z | 194.287° SSW |
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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