STARLINK-35128, 65628
Orbit data source: Space-Track
STARLINK-35128, 65628 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 18 Sep 2025 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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65628 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-35128
1 65628U 25210G 26171.35846370 .00013040 00000-0 39627-3 0 9998
2 65628 53.1572 188.5300 0001056 98.0174 262.0948 15.34409750 43475Epoch: 2026-06-20T08:36Z
TLE epoch observation values (Epoch: 2026-06-20T08:36:11.263Z)
Latitude
-0.00007°
Longitude
150.90879°
Altitude
463.675 km
Speed
7.636 km/s
True Right ascension
12h 34m 07s
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
07:12:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.654 km
Perigee altitude
462.209 km
Semi-major axis
6,841.069 km
Eccentricity
0.00011
Inclination
53.1572°
RAAN
188.53°
Arg. of periapsis
98.0174°
True anomaly
262.08281°
Mean anomaly
262.0948°
Eccentric anomaly
262.08881°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00039627
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Other satellites on launch #210 in the year 2025 (2025-09-18 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-35128 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 | 2026-06-21 03:31:44.659Z | 211.318° SW | 2026-06-21 03:34:44.659Z | 134.523° SE | 38.835° | 2026-06-21 03:37:44.659Z | 60.208° ENE |
| 4 mins | 2026-06-21 05:10:44.659Z | 292.442° WNW | 2026-06-21 05:12:44.659Z | 338.326° N | 21.326° | 2026-06-21 05:14:44.659Z | 19.613° NNE |
| 5 mins | 2026-06-21 10:06:44.659Z | 333.048° NNW | 2026-06-21 10:08:44.659Z | 44.012° NE | 35.277° | 2026-06-21 10:11:44.659Z | 108.03° ESE |
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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