KUIPER-00124, 65953
Orbit data source: Space-Track
KUIPER-00124, 65953 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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65953 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-00124
1 65953U 25228G 26171.41362130 .00002500 00000-0 35681-3 0 9997
2 65953 51.8982 261.3206 0000536 106.3933 253.7088 14.79938661 38516Epoch: 2026-06-20T09:55Z
TLE epoch observation values (Epoch: 2026-06-20T09:55:36.880Z)
Latitude
-0.00003°
Longitude
-156.21169°
Altitude
630.37 km
Speed
7.544 km/s
True Right ascension
17h 25m 16s
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
07:15:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.345 km
Perigee altitude
629.594 km
Semi-major axis
7,008.106 km
Eccentricity
0.00005
Inclination
51.8982°
RAAN
261.3206°
Arg. of periapsis
106.3933°
True anomaly
253.7029°
Mean anomaly
253.7088°
Eccentric anomaly
253.70585°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00035681
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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-00124 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 07:08:49.464Z | 151.839° SSE | 2026-06-21 07:10:49.464Z | 124.435° SE | 13.455° | 2026-06-21 07:12:49.464Z | 97.586° ESE |
| 7 mins | 2026-06-21 08:48:49.464Z | 229.165° WSW | 2026-06-21 08:51:49.464Z | 72.112° E | 44.661° | 2026-06-21 08:55:49.464Z | 53.011° ENE |
| 6 mins | 2026-06-21 10:30:49.464Z | 292.643° NW | 2026-06-21 10:33:49.464Z | 346.571° N | 23.7° | 2026-06-21 10:36:49.464Z | 33.293° NE |
| 4 mins | 2026-06-21 12:14:49.464Z | 338.91° N | 2026-06-21 12:15:49.464Z | 354.79° N | 17.036° | 2026-06-21 12:18:49.464Z | 39.832° NE |
| 7 mins | 2026-06-21 13:55:49.464Z | 328.608° NNW | 2026-06-21 13:58:49.464Z | 22.35° NNE | 26.838° | 2026-06-21 14:02:49.464Z | 85.181° E |
| 7 mins | 2026-06-21 15:37:49.464Z | 298.029° NW | 2026-06-21 15:40:49.464Z | 203.574° SW | 42.01° | 2026-06-21 15:44:49.464Z | 140.858° 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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