KUIPER-00062, 64522
Orbit data source: Space-Track
KUIPER-00062, 64522 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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64522 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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00062
1 64522U 25134Y 26171.34583968 .00002361 00000-0 33853-3 0 9994
2 64522 51.8960 136.6385 0000633 68.4270 291.6760 14.79939359 55315Epoch: 2026-06-20T08:18Z
TLE epoch observation values (Epoch: 2026-06-20T08:18:00.548Z)
Latitude
0.00001°
Longitude
103.57444°
Altitude
630.098 km
Speed
7.545 km/s
True Right ascension
09h 06m 33s
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
07:14:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.411 km
Perigee altitude
629.524 km
Semi-major axis
7,008.104 km
Eccentricity
0.00006
Inclination
51.896°
RAAN
136.6385°
Arg. of periapsis
68.427°
True anomaly
291.66926°
Mean anomaly
291.676°
Eccentric anomaly
291.67263°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00033853
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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-00062 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 | 2026-06-20 23:02:32.149Z | 153.105° SSE | 2026-06-20 23:04:32.149Z | 123.765° SE | 15.083° | 2026-06-20 23:06:32.149Z | 95.73° ESE |
| 7 mins | 2026-06-21 00:42:32.149Z | 234.344° WSW | 2026-06-21 00:45:32.149Z | 25.29° NE | 44.514° | 2026-06-21 00:49:32.149Z | 51.409° ENE |
| 6 mins | 2026-06-21 02:24:32.149Z | 294.748° NW | 2026-06-21 02:27:32.149Z | 346.916° N | 22.806° | 2026-06-21 02:30:32.149Z | 33.141° NE |
| 4 mins | 2026-06-21 04:08:32.149Z | 339.372° N | 2026-06-21 04:09:32.149Z | 355.189° N | 17.091° | 2026-06-21 04:12:32.149Z | 40.697° NE |
| 7 mins | 2026-06-21 05:49:32.149Z | 327.997° NNW | 2026-06-21 05:52:32.149Z | 23.003° NE | 28.116° | 2026-06-21 05:56:32.149Z | 87.753° E |
| 7 mins | 2026-06-21 07:31:32.149Z | 294.636° NW | 2026-06-21 07:34:32.149Z | 206.132° SW | 40.072° | 2026-06-21 07:38:32.149Z | 144.545° 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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