STARLINK-1008, 44714
Orbit data source: Space-Track
STARLINK-1008, 44714 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 11 Nov 2019 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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44714 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, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-1008
1 44714U 19074B 26033.25994499 .00002302 00000-0 87642-4 0 9994
2 44714 53.1590 343.5412 0001495 68.4987 291.6173 15.31038895343448Epoch: 2026-02-02T06:14Z
TLE epoch observation values (Epoch: 2026-02-02T06:14:19.247Z)
Latitude
-0.00004°
Longitude
117.50319°
Altitude
473.234 km
Speed
7.631 km/s
True Right ascension
22h 54m 09s
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
17:00:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.992 km
Perigee altitude
471.944 km
Semi-major axis
6,851.105 km
Eccentricity
0.00015
Inclination
53.159°
RAAN
343.5412°
Arg. of periapsis
68.4987°
True anomaly
291.60137°
Mean anomaly
291.6173°
Eccentric anomaly
291.60934°
Mean motion
3.82739 °/min
Orbital period
94.06 mins
BSTAR
0.000087642
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Other satellites on launch #74 in the year 2019 (2019-11-11 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-1008 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 | 2026-02-02 23:41:01.529Z | 250.108° W | 2026-02-02 23:43:01.529Z | 327.438° NNW | 40.75° | 2026-02-02 23:46:01.529Z | 41.992° NE |
| 4 mins | 2026-02-03 04:38:01.529Z | 350.44° N | 2026-02-03 04:40:01.529Z | 34.07° NE | 18.903° | 2026-02-03 04:42:01.529Z | 70.056° E |
| 5 mins | 2026-02-03 06:16:01.529Z | 300.975° NW | 2026-02-03 06:18:01.529Z | 188.208° SSW | 42.967° | 2026-02-03 06:21:01.529Z | 138.728° SSE |
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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