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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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https://www.satcat.com/sats-embedded/48908?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

48908, 2021-059AF

Orbit

SSO

Country

US

Related business

Space Development Agency (US)

Manufacturer

Astro Digital

Mission

Operational Defense Communications

Bus & Motor

CORVUS-XL, Unknown motor

Mass

23 kg wet, 23 kg dry

Launch date (UTC)

2021-06-30 (5 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

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 & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 MANDRAKE 2 BAKER
1 48908U 21059AF  26044.46684943  .00025656  00000-0  41229-3 0  9991
2 48908  97.7006 227.4175 0004874  80.8988 279.2815 15.52995561258054

Epoch: 2026-02-13T11:12Z

TLE epoch observation values (Epoch: 2026-02-13T11:12:15.790Z)

Latitude

-0.00008°

Longitude

-84.15212°

Altitude

410.58 km

Speed

7.665 km/s

True Right ascension

15h 09m 40s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

20:53:49

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

408.227 km

Perigee altitude

401.615 km

Semi-major axis

6,783.058 km

Eccentricity

0.00049

Inclination

97.7006°

RAAN

227.4175°

Arg. of periapsis

80.8988°

True anomaly

279.22637°

Mean anomaly

279.2815°

Eccentric anomaly

279.25394°

Mean motion

3.88512 °/min

Orbital period

92.66 mins

BSTAR

0.00041229

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Other satellites on launch #59 in the year 2021 (2021-06-30 UTC)

AYAN-21, 48944 (Decayed)

W-CUBE, 48965 (Decayed)

ASTROCAST-0202, 48961 (Decayed)

UMBRA-2001, 48906 (Decayed)

FARADAY_PHOENIX, 48924

ASTROCAST-0203, 48955

SPACEBEE-104, 48890 (Decayed)

SPACEBEE-88, 48935 (Decayed)

SPACEBEE-94, 48937 (Decayed)

DEMO9(AURORA), 48956 (Decayed)

CENTAURI-4 (TYVAK-0211), 48898 (Decayed)

SPACEBEE-99, 48936 (Decayed)

KSF1-D, 48950 (Decayed)

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

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	2026-02-14 12:05:06.630Z	161.892° S	2026-02-14 12:07:06.630Z	102.998° ESE	44.394°	2026-02-14 12:10:06.630Z	350.302° N

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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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Check out MANDRAKE 2 BAKER, 48908 on other resources

View MANDRAKE 2 BAKER, 48908 on NASA - NSSDCA Website

View MANDRAKE 2 BAKER, 48908 on Heavens-Above

View MANDRAKE 2 BAKER, 48908 on Keep Track

View MANDRAKE 2 BAKER, 48908 on Celestrak

View MANDRAKE 2 BAKER, 48908 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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