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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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 MANDRAKE 2 BAKER
1 48908U 21059AF 25308.44183573 .00022154 00000-0 43536-3 0 9997
2 48908 97.6969 119.5164 0005164 83.3594 276.8243 15.47301660242409Epoch: 2025-11-04T10:36Z
TLE epoch observation values (Epoch: 2025-11-04T10:36:14.607Z)
Latitude
0.00003°
Longitude
-83.47327°
Altitude
427.326 km
Speed
7.655 km/s
True Right ascension
07h 58m 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
23:02:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
425.077 km
Perigee altitude
418.054 km
Semi-major axis
6,799.703 km
Eccentricity
0.00052
Inclination
97.6969°
RAAN
119.5164°
Arg. of periapsis
83.3594°
True anomaly
276.76554°
Mean anomaly
276.8243°
Eccentric anomaly
276.79492°
Mean motion
3.87087 °/min
Orbital period
93 mins
BSTAR
0.00043536
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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 | 2025-11-05 11:34:18.816Z | 166.026° S | 2025-11-05 11:36:18.816Z | 161.946° S | 43.248° | 2025-11-05 11:39:18.816Z | 348.16° N |
| 5 mins | 2025-11-06 00:25:18.816Z | 14.86° NNE | 2025-11-06 00:27:18.816Z | 114.51° SE | 44.845° | 2025-11-06 00:30:18.816Z | 191.218° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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