KUIPER-00055, 64515
Orbit data source: Space-Track
KUIPER-00055, 64515 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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64515 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-00055
1 64515U 25134R 26171.44434846 .00001754 00000-0 25902-3 0 9998
2 64515 51.9023 76.2948 0000883 100.6025 259.5037 14.79934374 56162Epoch: 2026-06-20T10:39Z
TLE epoch observation values (Epoch: 2026-06-20T10:39:51.706Z)
Latitude
-0.00003°
Longitude
7.67045°
Altitude
630.391 km
Speed
7.544 km/s
True Right ascension
05h 05m 10s
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
07:17:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.601 km
Perigee altitude
629.363 km
Semi-major axis
7,008.119 km
Eccentricity
0.00009
Inclination
51.9023°
RAAN
76.2948°
Arg. of periapsis
100.6025°
True anomaly
259.49375°
Mean anomaly
259.5037°
Eccentric anomaly
259.49873°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00025902
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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-00055 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 20:33:46.810Z | 226.101° WSW | 2026-06-20 20:37:46.810Z | 125.319° SE | 44.53° | 2026-06-20 20:41:46.810Z | 54.534° ENE |
| 6 mins | 2026-06-20 22:16:46.810Z | 289.533° WNW | 2026-06-20 22:19:46.810Z | 343.703° N | 24.613° | 2026-06-20 22:22:46.810Z | 32.495° NE |
| 4 mins | 2026-06-21 00:00:46.810Z | 336.853° NNW | 2026-06-21 00:01:46.810Z | 352.562° N | 16.922° | 2026-06-21 00:04:46.810Z | 37.892° NE |
| 6 mins | 2026-06-21 01:42:46.810Z | 339.277° N | 2026-06-21 01:44:46.810Z | 19.027° NNE | 25.781° | 2026-06-21 01:48:46.810Z | 82.322° E |
| 7 mins | 2026-06-21 03:23:46.810Z | 301.208° NW | 2026-06-21 03:26:46.810Z | 212.84° SW | 43.508° | 2026-06-21 03:30:46.810Z | 137.82° SSE |
| 5 mins | 2026-06-21 19:14:46.810Z | 171.559° S | 2026-06-21 19:16:46.810Z | 133.095° SE | 24.613° | 2026-06-21 19:19:46.810Z | 80.94° 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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