STARLINK-31484, 59005
Orbit data source: Space-Track
STARLINK-31484, 59005 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 23 Feb 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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59005 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-31484
1 59005U 24036H 26171.41245089 -.00000514 00000-0 -52144-5 0 9997
2 59005 53.1612 320.7733 0001301 89.3351 270.7799 15.30189881131053Epoch: 2026-06-20T09:53Z
TLE epoch observation values (Epoch: 2026-06-20T09:53:55.756Z)
Latitude
-0.00003°
Longitude
-96.33648°
Altitude
476.133 km
Speed
7.629 km/s
True Right ascension
21h 23m 05s
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
21:23:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.393 km
Perigee altitude
474.61 km
Semi-major axis
6,853.639 km
Eccentricity
0.00013
Inclination
53.1612°
RAAN
320.7733°
Arg. of periapsis
89.3351°
True anomaly
270.76499°
Mean anomaly
270.7799°
Eccentric anomaly
270.77245°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.0000052144
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Other satellites on launch #36 in the year 2024 (2024-02-23 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-31484 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 | 2026-06-22 12:14:40.047Z | 229.82° WSW | 2026-06-22 12:17:40.047Z | 33.396° NE | 44.833° | 2026-06-22 12:20:40.047Z | 49.576° ENE |
| 5 mins | 2026-06-22 18:50:40.047Z | 316.415° NNW | 2026-06-22 18:52:40.047Z | 48.517° ENE | 44.152° | 2026-06-22 18:55:40.047Z | 124.791° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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