STARLINK-36490, 67305
Orbit data source: Space-Track
STARLINK-36490, 67305 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 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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67305 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
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-36490
1 67305U 26002A 26062.15984211 .00030520 00000-0 11132-2 0 9998
2 67305 43.0053 1.8507 0002896 250.3763 109.6777 15.27600975 10145Epoch: 2026-03-03T03:50Z
TLE epoch observation values (Epoch: 2026-03-03T03:50:10.358Z)
Latitude
0.00004°
Longitude
143.36469°
Altitude
483.432 km
Speed
7.625 km/s
True Right ascension
00h 07m 24s
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
09:13:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.918 km
Perigee altitude
482.943 km
Semi-major axis
6,863.068 km
Eccentricity
0.00029
Inclination
43.0053°
RAAN
1.8507°
Arg. of periapsis
250.3763°
True anomaly
109.70894°
Mean anomaly
109.6777°
Eccentric anomaly
109.69332°
Mean motion
3.81738 °/min
Orbital period
94.31 mins
BSTAR
0.0011132
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Other satellites on launch #2 in the year 2026 (2026-01-04 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-36490 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 05:28:05.169Z | 255.969° W | 2026-03-04 05:30:05.169Z | 218.211° SW | 18.912° | 2026-03-04 05:32:05.169Z | 178.326° S |
| 4 mins | 2026-03-04 22:25:05.169Z | 190.445° SSW | 2026-03-04 22:27:05.169Z | 137.313° SSE | 25.453° | 2026-03-04 22:29:05.169Z | 95.757° ESE |
| 6 mins | 2026-03-05 00:03:05.169Z | 259.505° W | 2026-03-05 00:05:05.169Z | 285.752° WNW | 42.659° | 2026-03-05 00:09:05.169Z | 70.938° E |
| 6 mins | 2026-03-05 01:42:05.169Z | 289.931° WNW | 2026-03-05 01:45:05.169Z | 28.841° NE | 36.776° | 2026-03-05 01:48:05.169Z | 78.801° E |
| 6 mins | 2026-03-05 03:21:05.169Z | 287.085° WNW | 2026-03-05 03:24:05.169Z | 127.343° SE | 43.715° | 2026-03-05 03:27:05.169Z | 111.959° ESE |
| 4 mins | 2026-03-05 05:01:05.169Z | 242.938° WSW | 2026-03-05 05:02:05.169Z | 221.732° SW | 19.269° | 2026-03-05 05:05:05.169Z | 166.942° 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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