STARLINK-1080, 44961
Orbit data source: Space-Track
STARLINK-1080, 44961 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 Jan 2020 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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44961 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
260 kg wet, ~248 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 4.4 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-1080
1 44961U 20001AZ 25258.60071743 .00000849 00000-0 75902-4 0 9995
2 44961 53.0557 12.6238 0001060 98.2601 261.8508 15.06391747314029Epoch: 2025-09-15T14:25Z
TLE epoch observation values (Epoch: 2025-09-15T14:25:01.985Z)
Latitude
-0.00006°
Longitude
161.56244°
Altitude
548.22 km
Speed
7.589 km/s
True Right ascension
00h 50m 29s
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
18:20:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.241 km
Perigee altitude
546.773 km
Semi-major axis
6,925.644 km
Eccentricity
0.00011
Inclination
53.0557°
RAAN
12.6238°
Arg. of periapsis
98.2601°
True anomaly
261.83878°
Mean anomaly
261.8508°
Eccentric anomaly
261.84479°
Mean motion
3.76576 °/min
Orbital period
95.6 mins
BSTAR
0.000075902
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Other satellites on launch #1 in the year 2020 (2020-01-07 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.STARLINK-1080 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 09:41:03.082Z | 193.314° SSW | 2025-09-16 09:44:03.082Z | 129.431° SE | 30.28° | 2025-09-16 09:47:03.082Z | 70.105° E |
| 6 mins | 2025-09-16 11:21:03.082Z | 272.794° WNW | 2025-09-16 11:23:03.082Z | 314.769° NW | 29.537° | 2025-09-16 11:27:03.082Z | 35.773° NE |
| 6 mins | 2025-09-16 16:23:03.082Z | 333.763° NNW | 2025-09-16 16:25:03.082Z | 21.783° NNE | 32.394° | 2025-09-16 16:29:03.082Z | 102.303° ESE |
| 5 mins | 2025-09-16 18:03:03.082Z | 270.05° WNW | 2025-09-16 18:05:03.082Z | 219.476° SW | 26.584° | 2025-09-16 18:08:03.082Z | 168.935° S |
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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