LINCS1, 48902 (Decayed)
Orbit data source: Space-Track
LINCS1, 48902 was an American payload satellite in LEO 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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48902 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
GA-EMS
Mission
Decayed Defense Communications
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.7 m
Radar Cross Section
0.218 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 LINCS1
1 48902U 21059Z 25067.90029484 .08818599 26881-5 70042-3 0 9990
2 48902 97.6367 241.3248 0010798 275.7747 84.2321 16.39906497206328Epoch: 2025-03-08T21:36Z
TLE epoch observation values (Epoch: 2025-03-08T21:36:25.474Z)
Latitude
0.00005°
Longitude
110.37898°
Altitude
168.592 km
Speed
7.805 km/s
True Right ascension
16h 05m 17s
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
15:52:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
169.933 km
Perigee altitude
155.807 km
Semi-major axis
6,541.007 km
Eccentricity
0.00108
Inclination
97.6367°
RAAN
241.3248°
Arg. of periapsis
275.7747°
True anomaly
84.35523°
Mean anomaly
84.2321°
Eccentric anomaly
84.29366°
Mean motion
4.10276 °/min
Orbital period
87.75 mins
BSTAR
0.00070042
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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.LINCS1 Visibility
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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. |
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| This satellite is decayed. |
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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