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: 5 hours ago
TLE from 5 hours ago
0 MANDRAKE 2 BAKER
1 48908U 21059AF 26095.25872893 .00032717 00000-0 47105-3 0 9992
2 48908 97.7030 282.0437 0003093 243.0664 117.0274 15.55979516265944Epoch: 2026-04-05T06:12Z
TLE epoch observation values (Epoch: 2026-04-05T06:12:34.179Z)
Latitude
-0.00002°
Longitude
-4.66544°
Altitude
403.39 km
Speed
7.668 km/s
True Right ascension
18h 48m 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
17:00:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
398.333 km
Perigee altitude
394.143 km
Semi-major axis
6,774.375 km
Eccentricity
0.00031
Inclination
97.703°
RAAN
282.0437°
Arg. of periapsis
243.0664°
True anomaly
117.05897°
Mean anomaly
117.0274°
Eccentric anomaly
117.04318°
Mean motion
3.8926 °/min
Orbital period
92.48 mins
BSTAR
0.00047105
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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 | 2026-04-05 12:31:06.082Z | 173.514° S | 2026-04-05 12:33:06.082Z | 217.365° SW | 43.357° | 2026-04-05 12:36:06.082Z | 343.804° N |
| 4 mins | 2026-04-06 01:18:06.082Z | 13.825° NNE | 2026-04-06 01:20:06.082Z | 186.095° SSW | 42.745° | 2026-04-06 01:22:06.082Z | 192.042° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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