STARLINK-5153, 54088
Orbit data source: Space-Track
STARLINK-5153, 54088 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 20 Oct 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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54088 intel report (Beta)
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Edit Public Description
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, 4.4 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 STARLINK-5153
1 54088U 22136AP 25260.67769601 .00000054 00000-0 21496-4 0 9991
2 54088 53.2189 30.9071 0000862 90.4572 269.6519 15.08838765160868Epoch: 2025-09-17T16:15Z
TLE epoch observation values (Epoch: 2025-09-17T16:15:52.935Z)
Latitude
-0.00001°
Longitude
150.08632°
Altitude
540.648 km
Speed
7.593 km/s
True Right ascension
02h 03m 37s
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
05:01:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.588 km
Perigee altitude
539.396 km
Semi-major axis
6,918.129 km
Eccentricity
0.00009
Inclination
53.2189°
RAAN
30.9071°
Arg. of periapsis
90.4572°
True anomaly
269.64202°
Mean anomaly
269.6519°
Eccentric anomaly
269.64696°
Mean motion
3.7719 °/min
Orbital period
95.44 mins
BSTAR
0.000021496
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Other satellites on launch #136 in the year 2022 (2022-10-20 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-5153 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 | 2025-09-18 13:12:05.370Z | 296.829° NW | 2025-09-18 13:14:05.370Z | 331.152° NNW | 19.084° | 2025-09-18 13:17:05.370Z | 23.543° NE |
| 4 mins | 2025-09-18 16:34:05.370Z | 350.947° N | 2025-09-18 16:36:05.370Z | 29.979° NE | 18.702° | 2025-09-18 16:38:05.370Z | 63.365° ENE |
| 6 mins | 2025-09-18 18:13:05.370Z | 312.106° NW | 2025-09-18 18:15:05.370Z | 323.674° NNW | 43.346° | 2025-09-18 18:19:05.370Z | 129.125° SE |
| 6 mins | 2025-09-19 11:23:05.370Z | 240.418° WSW | 2025-09-19 11:26:05.370Z | 343.012° N | 42.855° | 2025-09-19 11:29:05.370Z | 44.194° NE |
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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