STARLINK-36246, 67939
Orbit data source: Space-Track
STARLINK-36246, 67939 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 24 Feb 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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67939 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 STARLINK-36246
1 67939U 26037H 26171.43742501 .00013912 00000-0 51394-3 0 9996
2 67939 43.0059 330.5633 0001491 261.7046 98.3636 15.27592787 19054Epoch: 2026-06-20T10:29Z
TLE epoch observation values (Epoch: 2026-06-20T10:29:53.520Z)
Latitude
-0.00008°
Longitude
-95.56185°
Altitude
482.936 km
Speed
7.626 km/s
True Right ascension
22h 02m 15s
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
07:13:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.978 km
Perigee altitude
483.932 km
Semi-major axis
6,863.092 km
Eccentricity
0.00015
Inclination
43.0059°
RAAN
330.5633°
Arg. of periapsis
261.7046°
True anomaly
98.3805°
Mean anomaly
98.3636°
Eccentric anomaly
98.37205°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.00051394
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Other satellites on launch #37 in the year 2026 (2026-02-24 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-36246 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 20:26:09.065Z | 256.555° W | 2026-06-20 20:28:09.065Z | 217.755° SW | 19.772° | 2026-06-20 20:30:09.065Z | 176.715° S |
| 4 mins | 2026-06-21 13:23:09.065Z | 189.456° SSW | 2026-06-21 13:25:09.065Z | 138.718° SSE | 24.559° | 2026-06-21 13:27:09.065Z | 97.147° ESE |
| 6 mins | 2026-06-21 15:01:09.065Z | 257.802° W | 2026-06-21 15:03:09.065Z | 278.344° WNW | 42.579° | 2026-06-21 15:07:09.065Z | 71.05° E |
| 6 mins | 2026-06-21 16:40:09.065Z | 289.23° WNW | 2026-06-21 16:43:09.065Z | 26.473° NE | 36.875° | 2026-06-21 16:46:09.065Z | 78.006° E |
| 6 mins | 2026-06-21 18:19:09.065Z | 287.703° WNW | 2026-06-21 18:22:09.065Z | 118.968° SE | 44.104° | 2026-06-21 18:25:09.065Z | 110.493° ESE |
| 4 mins | 2026-06-21 19:59:09.065Z | 244.739° WSW | 2026-06-21 20:00:09.065Z | 223.248° SW | 20.023° | 2026-06-21 20:03:09.065Z | 166.146° S |
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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