STARLINK-5360, 54846
Orbit data source: Space-Track
STARLINK-5360, 54846 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 28 Dec 2022 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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54846 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
305 kg wet, ~290 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-5360
1 54846U 22177AC 26171.34725935 -.00002069 00000-0 -65706-4 0 9998
2 54846 43.0031 272.8783 0001411 231.4239 128.6486 15.27562277192661Epoch: 2026-06-20T08:20Z
TLE epoch observation values (Epoch: 2026-06-20T08:20:03.207Z)
Latitude
-0.00006°
Longitude
-120.69831°
Altitude
483.483 km
Speed
7.625 km/s
True Right ascension
18h 11m 30s
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
23:18:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.015 km
Perigee altitude
484.078 km
Semi-major axis
6,863.184 km
Eccentricity
0.00014
Inclination
43.0031°
RAAN
272.8783°
Arg. of periapsis
231.4239°
True anomaly
128.66123°
Mean anomaly
128.6486°
Eccentric anomaly
128.65491°
Mean motion
3.81729 °/min
Orbital period
94.31 mins
BSTAR
-0.000065706
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Other satellites on launch #177 in the year 2022 (2022-12-28 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-5360 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 12:28:21.106Z | 287.338° WNW | 2026-06-22 12:31:21.106Z | 2.645° NNE | 38.119° | 2026-06-22 12:34:21.106Z | 76.829° E |
| 5 mins | 2026-06-22 14:08:21.106Z | 286.573° WNW | 2026-06-22 14:10:21.106Z | 246.83° WSW | 44.734° | 2026-06-22 14:13:21.106Z | 112.173° ESE |
| 4 mins | 2026-06-22 15:47:21.106Z | 250.514° W | 2026-06-22 15:49:21.106Z | 208.685° SW | 19.237° | 2026-06-22 15:51:21.106Z | 172.06° S |
| 4 mins | 2026-06-23 08:44:21.106Z | 183.907° SSW | 2026-06-23 08:45:21.106Z | 158.647° S | 24.9° | 2026-06-23 08:48:21.106Z | 92.881° ESE |
| 5 mins | 2026-06-23 10:22:21.106Z | 259.452° W | 2026-06-23 10:24:21.106Z | 320.53° NNW | 44.343° | 2026-06-23 10:27:21.106Z | 70.05° E |
| 5 mins | 2026-06-23 12:01:21.106Z | 291.949° WNW | 2026-06-23 12:03:21.106Z | 344.091° N | 37.533° | 2026-06-23 12:06:21.106Z | 74.852° E |
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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