STARLINK-36523, 67460
Orbit data source: Space-Track
STARLINK-36523, 67460 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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67460 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 + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-36523
1 67460U 26008R 26271.58335648 .00034675 00000-0 12648-2 0 9997
2 67460 43.0016 139.6854 0001460 265.2150 278.6664 15.27550619 5877Epoch: 2026-09-28T14:00Z
TLE epoch observation values (Epoch: 2026-09-28T14:00:01.999Z)
Latitude
-2.70878°
Longitude
105.20842°
Altitude
483.153 km
Speed
7.626 km/s
True Right ascension
21h 30m 18s
True Declination
-2° 41' 31"
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
16:59:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.084 km
Perigee altitude
484.08 km
Semi-major axis
6,863.219 km
Eccentricity
0.00015
Inclination
43.0016°
RAAN
139.6854°
Arg. of periapsis
265.215°
True anomaly
278.64986°
Mean anomaly
278.6664°
Eccentric anomaly
278.65813°
Mean motion
3.81726 °/min
Orbital period
94.31 mins
BSTAR
0.0012648
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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-36523 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-29 00:40:42.145Z | 269.802° W | 2026-09-29 00:43:42.145Z | 202.027° SSW | 31.154° | 2026-09-29 00:46:42.145Z | 148.325° SSE |
| 4 mins | 2026-09-29 17:38:42.145Z | 170.618° S | 2026-09-29 17:39:42.145Z | 150.684° SSE | 18.776° | 2026-09-29 17:42:42.145Z | 97.842° ESE |
| 5 mins | 2026-09-29 19:16:42.145Z | 243.084° WSW | 2026-09-29 19:18:42.145Z | 127.669° SE | 78.476° | 2026-09-29 19:21:42.145Z | 73.234° E |
| 5 mins | 2026-09-29 20:55:42.145Z | 289.98° WNW | 2026-09-29 20:57:42.145Z | 358.078° N | 51.668° | 2026-09-29 21:00:42.145Z | 71.48° E |
| 5 mins | 2026-09-29 22:34:42.145Z | 293.537° NW | 2026-09-29 22:36:42.145Z | 348.116° N | 70.482° | 2026-09-29 22:39:42.145Z | 98.171° 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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