STARLINK-31315, 58884
Orbit data source: Space-Track
STARLINK-31315, 58884 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 29 Jan 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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58884 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: 2 days ago
TLE from 2 days ago
0 STARLINK-31315
1 58884U 24020J 26171.29246115 .00000440 00000-0 26978-4 0 9992
2 58884 53.1594 179.8881 0001395 82.4552 277.6608 15.30194470134141Epoch: 2026-06-20T07:01Z
TLE epoch observation values (Epoch: 2026-06-20T07:01:08.643Z)
Latitude
0.00005°
Longitude
166.09295°
Altitude
476.004 km
Speed
7.629 km/s
True Right ascension
11h 59m 33s
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
00:36:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.444 km
Perigee altitude
474.532 km
Semi-major axis
6,853.625 km
Eccentricity
0.00014
Inclination
53.1594°
RAAN
179.8881°
Arg. of periapsis
82.4552°
True anomaly
277.64496°
Mean anomaly
277.6608°
Eccentric anomaly
277.65288°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.000026978
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Other satellites on launch #20 in the year 2024 (2024-01-29 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-31315 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 | 2026-06-23 02:36:48.451Z | 230.891° WSW | 2026-06-23 02:39:48.451Z | 40.976° NE | 42.823° | 2026-06-23 02:42:48.451Z | 49.304° ENE |
| 4 mins | 2026-06-23 07:33:48.451Z | 341.034° N | 2026-06-23 07:35:48.451Z | 15.909° NNE | 16.324° | 2026-06-23 07:37:48.451Z | 54.028° ENE |
| 6 mins | 2026-06-23 09:11:48.451Z | 313.77° NW | 2026-06-23 09:14:48.451Z | 97.298° ESE | 42.882° | 2026-06-23 09:17:48.451Z | 126.067° SE |
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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