KUIPER-00125, 65954
Orbit data source: Space-Track
KUIPER-00125, 65954 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 14 Oct 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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65954 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00125
1 65954U 25228H 26171.42980436 .00002154 00000-0 31140-3 0 9995
2 65954 51.8993 246.2895 0000489 107.2965 252.8051 14.79940444 38722Epoch: 2026-06-20T10:18Z
TLE epoch observation values (Epoch: 2026-06-20T10:18:55.096Z)
Latitude
-0.00002°
Longitude
-177.08463°
Altitude
630.36 km
Speed
7.544 km/s
True Right ascension
16h 25m 09s
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
07:17:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.306 km
Perigee altitude
629.621 km
Semi-major axis
7,008.1 km
Eccentricity
0.00005
Inclination
51.8993°
RAAN
246.2895°
Arg. of periapsis
107.2965°
True anomaly
252.79975°
Mean anomaly
252.8051°
Eccentric anomaly
252.80242°
Mean motion
3.6995 °/min
Orbital period
97.31 mins
BSTAR
0.0003114
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Other satellites on launch #228 in the year 2025 (2025-10-14 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.KUIPER-00125 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 07:33:22.167Z | 218.86° SW | 2026-06-21 07:37:22.167Z | 110.783° ESE | 42.029° | 2026-06-21 07:41:22.167Z | 57.171° ENE |
| 6 mins | 2026-06-21 09:16:22.167Z | 289.022° WNW | 2026-06-21 09:18:22.167Z | 325.783° NNW | 26.171° | 2026-06-21 09:22:22.167Z | 35.743° NE |
| 5 mins | 2026-06-21 10:59:22.167Z | 326.578° NNW | 2026-06-21 11:01:22.167Z | 357.246° N | 17.187° | 2026-06-21 11:04:22.167Z | 40.064° NE |
| 6 mins | 2026-06-21 12:41:22.167Z | 331.774° NNW | 2026-06-21 12:44:22.167Z | 25.452° NE | 23.955° | 2026-06-21 12:47:22.167Z | 73.055° E |
| 7 mins | 2026-06-21 14:23:22.167Z | 305.915° NW | 2026-06-21 14:26:22.167Z | 150.12° SSE | 44.194° | 2026-06-21 14:30:22.167Z | 131.281° 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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