STARLINK-36439, 67624
Orbit data source: Space-Track
STARLINK-36439, 67624 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 30 Jan 2026 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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67624 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 17.7 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 STARLINK-36439
1 67624U 26020H 26071.91668981 -.01899238 00000-0 -31893-1 0 9996
2 67624 43.0000 122.9678 0001179 268.1503 353.5246 15.54467521 6028Epoch: 2026-03-12T22:00Z
TLE epoch observation values (Epoch: 2026-03-12T22:00:01.999Z)
Latitude
-42.60094°
Longitude
-118.89521°
Altitude
416.005 km
Speed
7.662 km/s
True Right ascension
01h 26m 41s
True Declination
-42° 25' 16"
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
12:48:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
406.469 km
Perigee altitude
404.869 km
Semi-major axis
6,783.806 km
Eccentricity
0.00012
Inclination
43°
RAAN
122.9678°
Arg. of periapsis
268.1503°
True anomaly
353.52308°
Mean anomaly
353.5246°
Eccentric anomaly
353.52384°
Mean motion
3.88448 °/min
Orbital period
92.68 mins
BSTAR
-0.031893
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Other satellites on launch #20 in the year 2026 (2026-01-30 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.STARLINK-36439 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 | 2026-03-13 09:34:03.244Z | 288.222° WNW | 2026-03-13 09:36:03.244Z | 329.639° NNW | 34.031° | 2026-03-13 09:39:03.244Z | 71.725° E |
| 5 mins | 2026-03-13 11:12:03.244Z | 290.15° WNW | 2026-03-13 11:14:03.244Z | 22.735° NE | 44.816° | 2026-03-13 11:17:03.244Z | 105.96° ESE |
| 5 mins | 2026-03-14 07:07:03.244Z | 240.012° WSW | 2026-03-14 07:09:03.244Z | 163.123° S | 43.702° | 2026-03-14 07:12:03.244Z | 74.538° E |
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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