KUIPER-00065, 64525
Orbit data source: Space-Track
KUIPER-00065, 64525 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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64525 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-00065
1 64525U 25134AB 26171.33507387 .00002060 00000-0 29910-3 0 9992
2 64525 51.9024 146.8182 0000882 95.9659 264.1404 14.79933556 55155Epoch: 2026-06-20T08:02Z
TLE epoch observation values (Epoch: 2026-06-20T08:02:30.382Z)
Latitude
-0.00001°
Longitude
117.64043°
Altitude
630.344 km
Speed
7.544 km/s
True Right ascension
09h 47m 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
07:16:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.603 km
Perigee altitude
629.367 km
Semi-major axis
7,008.122 km
Eccentricity
0.00009
Inclination
51.9024°
RAAN
146.8182°
Arg. of periapsis
95.9659°
True anomaly
264.13035°
Mean anomaly
264.1404°
Eccentric anomaly
264.13537°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.0002991
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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-00065 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 | 2026-06-21 00:23:39.746Z | 196.762° SSW | 2026-06-21 00:27:39.746Z | 130.044° SE | 29.63° | 2026-06-21 00:31:39.746Z | 68.157° E |
| 7 mins | 2026-06-21 02:05:39.746Z | 262.328° W | 2026-06-21 02:08:39.746Z | 318.229° NNW | 34.818° | 2026-06-21 02:12:39.746Z | 40.318° NE |
| 4 mins | 2026-06-21 03:49:39.746Z | 322.756° NNW | 2026-06-21 03:51:39.746Z | 356.46° N | 18.362° | 2026-06-21 03:53:39.746Z | 27.09° NE |
| 4 mins | 2026-06-21 05:32:39.746Z | 346.822° N | 2026-06-21 05:33:39.746Z | 3.989° NNE | 19.373° | 2026-06-21 05:36:39.746Z | 52.958° ENE |
| 7 mins | 2026-06-21 07:13:39.746Z | 322.065° NNW | 2026-06-21 07:16:39.746Z | 48.948° ENE | 38.999° | 2026-06-21 07:20:39.746Z | 110.762° ESE |
| 5 mins | 2026-06-21 08:55:39.746Z | 267.098° W | 2026-06-21 08:57:39.746Z | 228.097° WSW | 23.988° | 2026-06-21 09:00:39.746Z | 178.662° S |
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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