STARLINK-36485, 67312
Orbit data source: Space-Track
STARLINK-36485, 67312 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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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-36485
1 67312U 26002H 26062.15341687 .00034535 00000-0 12574-2 0 9991
2 67312 43.0060 1.7996 0002226 242.4537 117.6089 15.27610105 10084Epoch: 2026-03-03T03:40Z
TLE epoch observation values (Epoch: 2026-03-03T03:40:55.217Z)
Latitude
-0°
Longitude
145.63296°
Altitude
483.443 km
Speed
7.625 km/s
True Right ascension
00h 07m 11s
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
09:13:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.431 km
Perigee altitude
483.375 km
Semi-major axis
6,863.04 km
Eccentricity
0.00022
Inclination
43.006°
RAAN
1.7996°
Arg. of periapsis
242.4537°
True anomaly
117.6315°
Mean anomaly
117.6089°
Eccentric anomaly
117.6202°
Mean motion
3.81741 °/min
Orbital period
94.3 mins
BSTAR
0.0012574
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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-36485 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 | 2026-03-04 22:14:12.910Z | 200.635° SSW | 2026-03-04 22:17:12.910Z | 142.353° SSE | 22.92° | 2026-03-04 22:19:12.910Z | 100.45° ESE |
| 6 mins | 2026-03-04 23:53:12.910Z | 254.473° W | 2026-03-04 23:56:12.910Z | 59.987° ENE | 42.432° | 2026-03-04 23:59:12.910Z | 71.362° E |
| 5 mins | 2026-03-05 01:33:12.910Z | 297.403° NW | 2026-03-05 01:35:12.910Z | 21.106° NNE | 37.193° | 2026-03-05 01:38:12.910Z | 76.475° E |
| 5 mins | 2026-03-05 03:12:12.910Z | 289.473° WNW | 2026-03-05 03:14:12.910Z | 92.549° ESE | 44.542° | 2026-03-05 03:17:12.910Z | 107.657° ESE |
| 4 mins | 2026-03-05 04:51:12.910Z | 247.972° W | 2026-03-05 04:52:12.910Z | 225.983° WSW | 21.499° | 2026-03-05 04:55:12.910Z | 164.306° S |
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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