KUIPER-00126, 65955
Orbit data source: Space-Track
KUIPER-00126, 65955 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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65955 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-00126
1 65955U 25228J 26171.44200443 .00002570 00000-0 36602-3 0 9991
2 65955 51.8997 266.2245 0000511 96.8035 263.2986 14.79934666 38446Epoch: 2026-06-20T10:36Z
TLE epoch observation values (Epoch: 2026-06-20T10:36:29.182Z)
Latitude
0.00001°
Longitude
-161.55366°
Altitude
630.319 km
Speed
7.544 km/s
True Right ascension
17h 44m 53s
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
07:15:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.34 km
Perigee altitude
629.623 km
Semi-major axis
7,008.119 km
Eccentricity
0.00005
Inclination
51.8997°
RAAN
266.2245°
Arg. of periapsis
96.8035°
True anomaly
263.29278°
Mean anomaly
263.2986°
Eccentric anomaly
263.29569°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00036602
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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-00126 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 | 2026-06-21 07:49:51.384Z | 168.105° S | 2026-06-21 07:51:51.384Z | 137.452° SSE | 19.508° | 2026-06-21 07:54:51.384Z | 88.639° E |
| 7 mins | 2026-06-21 09:30:51.384Z | 247.991° W | 2026-06-21 09:33:51.384Z | 0.71° NNE | 41.486° | 2026-06-21 09:37:51.384Z | 48.122° ENE |
| 5 mins | 2026-06-21 11:13:51.384Z | 314.005° NW | 2026-06-21 11:15:51.384Z | 350.709° N | 20.78° | 2026-06-21 11:18:51.384Z | 34.394° NE |
| 4 mins | 2026-06-21 12:56:51.384Z | 342.432° N | 2026-06-21 12:57:51.384Z | 358.538° N | 17.589° | 2026-06-21 13:00:51.384Z | 44.761° NE |
| 7 mins | 2026-06-21 14:37:51.384Z | 327.11° NNW | 2026-06-21 14:40:51.384Z | 29.409° NE | 31.779° | 2026-06-21 14:44:51.384Z | 95.632° ESE |
| 6 mins | 2026-06-21 16:19:51.384Z | 284.603° WNW | 2026-06-21 16:21:51.384Z | 242.986° WSW | 33.847° | 2026-06-21 16:25:51.384Z | 157.471° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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