KUIPER-00050, 64510
Orbit data source: Space-Track
KUIPER-00050, 64510 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 23 Jun 2025 UTC via an ATLAS V 551 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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64510 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Partially 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: 14 hours ago
TLE from 14 hours ago
0 KUIPER-00050
1 64510U 25134L 26171.26613602 .00001272 00000-0 19581-3 0 9993
2 64510 51.9001 116.9635 0000782 73.7882 286.3167 14.79934338 55584Epoch: 2026-06-20T06:23Z
TLE epoch observation values (Epoch: 2026-06-20T06:23:14.152Z)
Latitude
0.00005°
Longitude
112.67134°
Altitude
630.124 km
Speed
7.545 km/s
True Right ascension
07h 47m 51s
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
07:16:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.531 km
Perigee altitude
629.435 km
Semi-major axis
7,008.12 km
Eccentricity
0.00008
Inclination
51.9001°
RAAN
116.9635°
Arg. of periapsis
73.7882°
True anomaly
286.3081°
Mean anomaly
286.3167°
Eccentric anomaly
286.3124°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00019581
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Other satellites on launch #134 in the year 2025 (2025-06-23 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-00050 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 | 2026-06-20 22:44:51.189Z | 210.424° SW | 2026-06-20 22:48:51.189Z | 145.433° SSE | 37.462° | 2026-06-20 22:52:51.189Z | 63.352° ENE |
| 6 mins | 2026-06-21 00:27:51.189Z | 277.566° WNW | 2026-06-21 00:30:51.189Z | 340.115° N | 29.779° | 2026-06-21 00:33:51.189Z | 34.066° NE |
| 4 mins | 2026-06-21 02:11:51.189Z | 333.177° NNW | 2026-06-21 02:12:51.189Z | 349.426° N | 17.405° | 2026-06-21 02:15:51.189Z | 34.373° NE |
| 5 mins | 2026-06-21 03:53:51.189Z | 339.728° N | 2026-06-21 03:55:51.189Z | 15.323° NNE | 21.814° | 2026-06-21 03:58:51.189Z | 64.102° ENE |
| 7 mins | 2026-06-21 05:34:51.189Z | 312.539° NW | 2026-06-21 05:37:51.189Z | 15.739° NNE | 43.934° | 2026-06-21 05:41:51.189Z | 121.512° SE |
| 4 mins | 2026-06-21 07:17:51.189Z | 251.547° W | 2026-06-21 07:18:51.189Z | 235.097° WSW | 17.361° | 2026-06-21 07:21:51.189Z | 191.708° SSW |
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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