STARLINK-32588, 61866
Orbit data source: Space-Track
STARLINK-32588, 61866 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 07 Nov 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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61866 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-32588
1 61866U 24202X 26266.54319494 -.00000018 00000-0 88595-5 0 9998
2 61866 43.0052 200.8860 0000945 275.9654 84.1090 15.27574736105592Epoch: 2026-09-23T13:02Z
TLE epoch observation values (Epoch: 2026-09-23T13:02:12.042Z)
Latitude
-0.00003°
Longitude
2.94298°
Altitude
482.774 km
Speed
7.626 km/s
True Right ascension
13h 23m 32s
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
20:47:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.658 km
Perigee altitude
484.361 km
Semi-major axis
6,863.146 km
Eccentricity
0.00009
Inclination
43.0052°
RAAN
200.886°
Arg. of periapsis
275.9654°
True anomaly
84.11977°
Mean anomaly
84.109°
Eccentric anomaly
84.11439°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.0000088595
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Other satellites on launch #202 in the year 2024 (2024-11-07 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-32588 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-24 03:36:00.890Z | 290.608° WNW | 2026-09-24 03:38:00.890Z | 351.892° N | 83.122° | 2026-09-24 03:41:00.890Z | 105.732° ESE |
| 4 mins | 2026-09-24 05:15:00.890Z | 253.759° W | 2026-09-24 05:17:00.890Z | 206.532° SW | 25.104° | 2026-09-24 05:19:00.890Z | 165.947° S |
| 4 mins | 2026-09-24 22:12:00.890Z | 177.537° S | 2026-09-24 22:13:00.890Z | 154.788° SSE | 23.451° | 2026-09-24 22:16:00.890Z | 95.201° ESE |
| 5 mins | 2026-09-24 23:50:00.890Z | 253.01° W | 2026-09-24 23:52:00.890Z | 337.534° N | 87.056° | 2026-09-24 23:55:00.890Z | 71.121° E |
| 5 mins | 2026-09-25 01:29:00.890Z | 291.463° WNW | 2026-09-25 01:31:00.890Z | 349.558° N | 50.385° | 2026-09-25 01:34:00.890Z | 72.725° E |
| 6 mins | 2026-09-25 03:08:00.890Z | 290.515° WNW | 2026-09-25 03:10:00.890Z | 311.719° NW | 72.311° | 2026-09-25 03:14:00.890Z | 105.643° ESE |
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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