STARLINK-36414, 67468
Orbit data source: Space-Track
STARLINK-36414, 67468 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 14 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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67468 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: 19 hours ago
TLE from 19 hours ago
0 STARLINK-36414
1 67468U 26008Z 26062.53121447 .00031052 00000-0 11324-2 0 9994
2 67468 42.9975 239.7032 0002096 286.0720 73.9901 15.27602804 8638Epoch: 2026-03-03T12:44Z
TLE epoch observation values (Epoch: 2026-03-03T12:44:56.930Z)
Latitude
0.00001°
Longitude
-112.84293°
Altitude
482.36 km
Speed
7.626 km/s
True Right ascension
15h 58m 48s
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
11:20:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.365 km
Perigee altitude
483.488 km
Semi-major axis
6,863.063 km
Eccentricity
0.00021
Inclination
42.9975°
RAAN
239.7032°
Arg. of periapsis
286.072°
True anomaly
74.01319°
Mean anomaly
73.9901°
Eccentric anomaly
74.00164°
Mean motion
3.81739 °/min
Orbital period
94.31 mins
BSTAR
0.0011324
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Other satellites on launch #8 in the year 2026 (2026-01-14 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-36414 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 | 2026-03-04 14:02:28.006Z | 181.558° SSW | 2026-03-04 14:04:28.006Z | 145.663° SSE | 17.116° | 2026-03-04 14:06:28.006Z | 108.272° ESE |
| 6 mins | 2026-03-04 15:40:28.006Z | 242.886° WSW | 2026-03-04 15:43:28.006Z | 105.129° ESE | 42.89° | 2026-03-04 15:46:28.006Z | 73.745° E |
| 5 mins | 2026-03-04 17:20:28.006Z | 291.757° WNW | 2026-03-04 17:22:28.006Z | 14.461° NNE | 37.866° | 2026-03-04 17:25:28.006Z | 72.832° E |
| 5 mins | 2026-03-04 18:59:28.006Z | 294.535° NW | 2026-03-04 19:01:28.006Z | 27.133° NE | 43.499° | 2026-03-04 19:04:28.006Z | 98.316° ESE |
| 5 mins | 2026-03-04 20:38:28.006Z | 257.812° W | 2026-03-04 20:40:28.006Z | 200.285° SSW | 28.195° | 2026-03-04 20:43:28.006Z | 146.443° 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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