STARLINK-31840, 60127
Orbit data source: Space-Track
STARLINK-31840, 60127 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 24 Jun 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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60127 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 STARLINK-31840
1 60127U 24118Q 25260.00338399 -.00001202 00000-0 -28479-4 0 9993
2 60127 53.1598 113.5156 0001340 72.6332 287.4815 15.30181240 69108Epoch: 2025-09-17T00:04Z
TLE epoch observation values (Epoch: 2025-09-17T00:04:52.376Z)
Latitude
-0.00005°
Longitude
116.11176°
Altitude
475.895 km
Speed
7.629 km/s
True Right ascension
07h 34m 03s
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
13:00:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.446 km
Perigee altitude
474.609 km
Semi-major axis
6,853.665 km
Eccentricity
0.00013
Inclination
53.1598°
RAAN
113.5156°
Arg. of periapsis
72.6332°
True anomaly
287.46685°
Mean anomaly
287.4815°
Eccentric anomaly
287.47418°
Mean motion
3.82524 °/min
Orbital period
94.11 mins
BSTAR
-0.000028479
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Other satellites on launch #118 in the year 2024 (2024-06-24 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-31840 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 | 2025-09-17 22:29:40.919Z | 350.846° N | 2025-09-17 22:31:40.919Z | 36.911° NE | 20.202° | 2025-09-17 22:33:40.919Z | 73.515° E |
| 5 mins | 2025-09-18 00:07:40.919Z | 294.799° NW | 2025-09-18 00:09:40.919Z | 197.149° SSW | 40.646° | 2025-09-18 00:12:40.919Z | 143.509° SSE |
| 5 mins | 2025-09-18 17:02:40.919Z | 247.209° WSW | 2025-09-18 17:04:40.919Z | 303.431° NW | 40.762° | 2025-09-18 17:07:40.919Z | 41.316° NE |
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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