STARLINK-32318, 61864
Orbit data source: Space-Track
STARLINK-32318, 61864 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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61864 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-32318
1 61864U 24202V 26266.15344671 -.00000314 00000-0 -18969-5 0 9996
2 61864 43.0036 203.1199 0001140 266.3043 93.7679 15.27573624105535Epoch: 2026-09-23T03:40Z
TLE epoch observation values (Epoch: 2026-09-23T03:40:57.795Z)
Latitude
0.00001°
Longitude
145.87045°
Altitude
482.895 km
Speed
7.626 km/s
True Right ascension
13h 32m 28s
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
20:46:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.795 km
Perigee altitude
484.23 km
Semi-major axis
6,863.15 km
Eccentricity
0.00011
Inclination
43.0036°
RAAN
203.1199°
Arg. of periapsis
266.3043°
True anomaly
93.78094°
Mean anomaly
93.7679°
Eccentric anomaly
93.77442°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
-0.0000018969
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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-32318 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-24 03:38:12.611Z | 288.54° WNW | 2026-09-24 03:42:12.611Z | 94.452° ESE | 76.971° | 2026-09-24 03:45:12.611Z | 107.686° ESE |
| 4 mins | 2026-09-24 05:19:12.611Z | 247.175° WSW | 2026-09-24 05:20:12.611Z | 224.899° SW | 23.415° | 2026-09-24 05:23:12.611Z | 163.993° S |
| 5 mins | 2026-09-24 22:15:12.611Z | 190.604° SSW | 2026-09-24 22:17:12.611Z | 146.694° SSE | 25.195° | 2026-09-24 22:20:12.611Z | 91.165° ESE |
| 6 mins | 2026-09-24 23:53:12.611Z | 254.366° W | 2026-09-24 23:56:12.611Z | 51.464° ENE | 73.719° | 2026-09-24 23:59:12.611Z | 70.92° E |
| 5 mins | 2026-09-25 01:33:12.611Z | 295.39° NW | 2026-09-25 01:35:12.611Z | 9.181° NNE | 50.465° | 2026-09-25 01:38:12.611Z | 75.045° E |
| 5 mins | 2026-09-25 03:12:12.611Z | 290.115° WNW | 2026-09-25 03:14:12.611Z | 7.525° NNE | 85.405° | 2026-09-25 03:17:12.611Z | 106.756° 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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