KUIPER-00041, 64502
Orbit data source: Space-Track
KUIPER-00041, 64502 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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64502 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: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00041
1 64502U 25134C 26171.39721786 .00002063 00000-0 29949-3 0 9999
2 64502 51.8974 151.4035 0000638 79.9020 280.2014 14.79930928 55106Epoch: 2026-06-20T09:31Z
TLE epoch observation values (Epoch: 2026-06-20T09:31:59.623Z)
Latitude
-0.00002°
Longitude
99.79262°
Altitude
630.209 km
Speed
7.545 km/s
True Right ascension
10h 05m 36s
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
07:15:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.441 km
Perigee altitude
629.547 km
Semi-major axis
7,008.131 km
Eccentricity
0.00006
Inclination
51.8974°
RAAN
151.4035°
Arg. of periapsis
79.902°
True anomaly
280.1942°
Mean anomaly
280.2014°
Eccentric anomaly
280.1978°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00029949
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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-00041 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 00:16:22.999Z | 168.071° S | 2026-06-21 00:18:22.999Z | 137.517° SSE | 19.431° | 2026-06-21 00:21:22.999Z | 88.76° E |
| 7 mins | 2026-06-21 01:57:22.999Z | 247.793° W | 2026-06-21 02:00:22.999Z | 0.69° NNE | 41.552° | 2026-06-21 02:04:22.999Z | 48.161° ENE |
| 5 mins | 2026-06-21 03:40:22.999Z | 313.89° NW | 2026-06-21 03:42:22.999Z | 350.618° N | 20.807° | 2026-06-21 03:45:22.999Z | 34.361° NE |
| 4 mins | 2026-06-21 05:23:22.999Z | 342.351° N | 2026-06-21 05:24:22.999Z | 358.449° N | 17.581° | 2026-06-21 05:27:22.999Z | 44.682° NE |
| 7 mins | 2026-06-21 07:04:22.999Z | 327.093° NNW | 2026-06-21 07:07:22.999Z | 29.216° NE | 31.736° | 2026-06-21 07:11:22.999Z | 95.517° ESE |
| 6 mins | 2026-06-21 08:46:22.999Z | 284.76° WNW | 2026-06-21 08:48:22.999Z | 243.287° WSW | 33.895° | 2026-06-21 08:52:22.999Z | 157.384° 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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