KUIPER-00127, 65956
Orbit data source: Space-Track
KUIPER-00127, 65956 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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65956 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: 15 hours ago
TLE from 15 hours ago
0 KUIPER-00127
1 65956U 25228K 26277.38752021 .00001655 00000-0 24610-3 0 9995
2 65956 51.9007 150.2047 0001178 93.2997 266.8100 14.79934081 54244Epoch: 2026-10-04T09:18Z
TLE epoch observation values (Epoch: 2026-10-04T09:18:01.746Z)
Latitude
-0.00001°
Longitude
-2.38408°
Altitude
630.325 km
Speed
7.544 km/s
True Right ascension
10h 00m 49s
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
17:52:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.809 km
Perigee altitude
629.158 km
Semi-major axis
7,008.12 km
Eccentricity
0.00012
Inclination
51.9007°
RAAN
150.2047°
Arg. of periapsis
93.2997°
True anomaly
266.79652°
Mean anomaly
266.81°
Eccentric anomaly
266.80326°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.0002461
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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-00127 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 | 2026-10-05 00:20:51.738Z | 317.295° NNW | 2026-10-05 00:24:51.738Z | 21.555° NNE | 44.996° | 2026-10-05 00:28:51.738Z | 101.065° ESE |
| 6 mins | 2026-10-05 02:03:51.738Z | 280.126° WNW | 2026-10-05 02:06:51.738Z | 215.496° SW | 33.556° | 2026-10-05 02:09:51.738Z | 167.136° S |
| 7 mins | 2026-10-05 17:53:51.738Z | 208.949° SW | 2026-10-05 17:56:51.738Z | 116.461° SE | 56.755° | 2026-10-05 18:00:51.738Z | 59.147° ENE |
| 6 mins | 2026-10-05 19:35:51.738Z | 286.552° WNW | 2026-10-05 19:37:51.738Z | 325.772° NNW | 31.93° | 2026-10-05 19:41:51.738Z | 36.527° NE |
| 5 mins | 2026-10-05 21:18:51.738Z | 326.502° NNW | 2026-10-05 21:20:51.738Z | 357.654° N | 18.182° | 2026-10-05 21:23:51.738Z | 39.507° NE |
| 6 mins | 2026-10-05 23:00:51.738Z | 332.884° NNW | 2026-10-05 23:03:51.738Z | 25.339° NE | 24.656° | 2026-10-05 23:06:51.738Z | 70.43° E |
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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