STARLINK-5628, 55466
Orbit data source: Space-Track
STARLINK-5628, 55466 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Feb 2023 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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55466 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, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-5628
1 55466U 23015T 25303.30016178 -.00000412 00000-0 -15404-4 0 9993
2 55466 43.0064 314.1781 0001326 269.4890 90.5801 15.02537280151148Epoch: 2025-10-30T07:12Z
TLE epoch observation values (Epoch: 2025-10-30T07:12:13.977Z)
Latitude
0.00001°
Longitude
167.25894°
Altitude
558.864 km
Speed
7.584 km/s
True Right ascension
20h 56m 42s
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
11:53:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.919 km
Perigee altitude
560.078 km
Semi-major axis
6,939.135 km
Eccentricity
0.00013
Inclination
43.0064°
RAAN
314.1781°
Arg. of periapsis
269.489°
True anomaly
90.59529°
Mean anomaly
90.5801°
Eccentric anomaly
90.5877°
Mean motion
3.75479 °/min
Orbital period
95.88 mins
BSTAR
-0.000015404
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Other satellites on launch #15 in the year 2023 (2023-02-02 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-5628 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 | 2025-10-31 04:09:02.176Z | 221.361° SW | 2025-10-31 04:12:02.176Z | 169.928° S | 34.445° | 2025-10-31 04:16:02.176Z | 80.829° E |
| 7 mins | 2025-10-31 05:50:02.176Z | 268.24° W | 2025-10-31 05:53:02.176Z | 345.705° N | 42.544° | 2025-10-31 05:57:02.176Z | 71.416° E |
| 7 mins | 2025-10-31 07:31:02.176Z | 290.593° WNW | 2025-10-31 07:34:02.176Z | 7.804° NNE | 40.59° | 2025-10-31 07:38:02.176Z | 86.981° E |
| 6 mins | 2025-10-31 09:12:02.176Z | 280.679° WNW | 2025-10-31 09:15:02.176Z | 182.213° SSW | 41.174° | 2025-10-31 09:18:02.176Z | 126.038° SE |
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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