STARLINK-36396, 67494
Orbit data source: Space-Track
STARLINK-36396, 67494 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 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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67494 intel report (Beta)
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Edit Public Description
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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-36396
1 67494U 26012B 26034.58335648 -.02476803 00000-0 -21043-1 0 9991
2 67494 42.9997 150.6696 0001448 281.3551 92.2032 15.71927561 3585Epoch: 2026-02-03T14:00Z
TLE epoch observation values (Epoch: 2026-02-03T14:00:01.999Z)
Latitude
9.20934°
Longitude
176.85496°
Altitude
352.469 km
Speed
7.7 km/s
True Right ascension
10h 42m 30s
True Declination
9° 09' 07"
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
07:22:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
356.346 km
Perigee altitude
354.396 km
Semi-major axis
6,733.508 km
Eccentricity
0.00014
Inclination
42.9997°
RAAN
150.6696°
Arg. of periapsis
281.3551°
True anomaly
92.21978°
Mean anomaly
92.2032°
Eccentric anomaly
92.21149°
Mean motion
3.92809 °/min
Orbital period
91.65 mins
BSTAR
-0.021043
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Other satellites on launch #12 in the year 2026 (2026-01-18 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-36396 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 | 2026-02-04 11:34:29.494Z | 237.008° WSW | 2026-02-04 11:36:29.494Z | 133.88° SE | 42.217° | 2026-02-04 11:38:29.494Z | 77.461° E |
| 4 mins | 2026-02-04 13:11:29.494Z | 296.155° NW | 2026-02-04 13:12:29.494Z | 335.316° NNW | 34.967° | 2026-02-04 13:15:29.494Z | 69.509° E |
| 4 mins | 2026-02-04 14:47:29.494Z | 296.17° NW | 2026-02-04 14:49:29.494Z | 27.496° NE | 40.79° | 2026-02-04 14:51:29.494Z | 90.465° ESE |
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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