KUIPER-00134, 65960
Orbit data source: Space-Track
KUIPER-00134, 65960 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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65960 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-00134
1 65960U 25228P 26277.56606020 .00020406 00000-0 54459-3 0 9996
2 65960 51.8715 26.5565 0004533 333.7993 26.2764 15.38091270 55975Epoch: 2026-10-04T13:35Z
TLE epoch observation values (Epoch: 2026-10-04T13:35:07.601Z)
Latitude
-0.00001°
Longitude
169.51735°
Altitude
449.741 km
Speed
7.645 km/s
True Right ascension
01h 46m 13s
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
17:51:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.318 km
Perigee altitude
449.125 km
Semi-major axis
6,830.358 km
Eccentricity
0.00045
Inclination
51.8715°
RAAN
26.5565°
Arg. of periapsis
333.7993°
True anomaly
26.29941°
Mean anomaly
26.2764°
Eccentric anomaly
26.2879°
Mean motion
3.84484 °/min
Orbital period
93.63 mins
BSTAR
0.00054459
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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-00134 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 | 2026-10-05 10:01:43.252Z | 223.019° SW | 2026-10-05 10:04:43.252Z | 184.368° SSW | 62.897° | 2026-10-05 10:07:43.252Z | 58.094° ENE |
| 4 mins | 2026-10-05 11:41:43.252Z | 309.655° NW | 2026-10-05 11:42:43.252Z | 333.319° NNW | 21.656° | 2026-10-05 11:45:43.252Z | 30.274° NE |
| 5 mins | 2026-10-05 16:35:43.252Z | 311.662° NW | 2026-10-05 16:37:43.252Z | 339.62° N | 70.842° | 2026-10-05 16:40:43.252Z | 123.677° 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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