STARLINK-31997, 60288
Orbit data source: Space-Track
STARLINK-31997, 60288 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 28 Jul 2024 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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60288 intel report (Beta)
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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, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-31997
1 60288U 24132L 26254.07149368 .00002529 00000-0 85990-4 0 9996
2 60288 53.1588 269.8983 0001078 83.1384 276.9742 15.34381734119966Epoch: 2026-09-11T01:42Z
TLE epoch observation values (Epoch: 2026-09-11T01:42:57.053Z)
Latitude
0.00002°
Longitude
-105.93952°
Altitude
463.569 km
Speed
7.636 km/s
True Right ascension
17h 59m 35s
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
02:53:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.752 km
Perigee altitude
462.277 km
Semi-major axis
6,841.152 km
Eccentricity
0.00011
Inclination
53.1588°
RAAN
269.8983°
Arg. of periapsis
83.1384°
True anomaly
276.96194°
Mean anomaly
276.9742°
Eccentric anomaly
276.96807°
Mean motion
3.83574 °/min
Orbital period
93.85 mins
BSTAR
0.00008599
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Other satellites on launch #132 in the year 2024 (2024-07-28 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-31997 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 | 2026-09-12 11:03:27.694Z | 297.478° NW | 2026-09-12 11:06:27.694Z | 247.066° WSW | 39.709° | 2026-09-12 11:09:27.694Z | 159.896° S |
| 4 mins | 2026-09-13 02:20:27.694Z | 164.459° S | 2026-09-13 02:22:27.694Z | 121.208° SE | 20.071° | 2026-09-13 02:24:27.694Z | 84.464° E |
| 5 mins | 2026-09-13 03:57:27.694Z | 260.685° W | 2026-09-13 03:59:27.694Z | 321.034° NNW | 45.304° | 2026-09-13 04:02:27.694Z | 36.68° NE |
| 4 mins | 2026-09-13 08:54:27.694Z | 358.824° N | 2026-09-13 08:55:27.694Z | 23.227° NE | 22.974° | 2026-09-13 08:58:27.694Z | 80.542° E |
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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