KUIPER-00048, 64508
Orbit data source: Space-Track
KUIPER-00048, 64508 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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64508 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: 15 hours ago
TLE from 15 hours ago
0 KUIPER-00048
1 64508U 25134J 26171.22697810 .00000839 00000-0 13909-3 0 9995
2 64508 51.8982 122.1504 0000911 91.4527 268.6540 14.79925580 55508Epoch: 2026-06-20T05:26Z
TLE epoch observation values (Epoch: 2026-06-20T05:26:50.907Z)
Latitude
-0.00001°
Longitude
131.99365°
Altitude
630.321 km
Speed
7.544 km/s
True Right ascension
08h 08m 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
07:12:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.649 km
Perigee altitude
629.372 km
Semi-major axis
7,008.148 km
Eccentricity
0.00009
Inclination
51.8982°
RAAN
122.1504°
Arg. of periapsis
91.4527°
True anomaly
268.64356°
Mean anomaly
268.654°
Eccentric anomaly
268.64878°
Mean motion
3.69946 °/min
Orbital period
97.31 mins
BSTAR
0.00013909
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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-00048 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 23:27:34.310Z | 222.39° SW | 2026-06-20 23:30:34.310Z | 165.822° S | 43.775° | 2026-06-20 23:34:34.310Z | 56.016° ENE |
| 5 mins | 2026-06-21 01:10:34.310Z | 297.465° NW | 2026-06-21 01:12:34.310Z | 337.766° N | 25.363° | 2026-06-21 01:15:34.310Z | 30.515° NE |
| 4 mins | 2026-06-21 02:53:34.310Z | 333.156° NNW | 2026-06-21 02:55:34.310Z | 5.235° NNE | 17.052° | 2026-06-21 02:57:34.310Z | 34.714° NE |
| 6 mins | 2026-06-21 04:35:34.310Z | 336.495° NNW | 2026-06-21 04:37:34.310Z | 13.098° NNE | 24.904° | 2026-06-21 04:41:34.310Z | 79.131° E |
| 7 mins | 2026-06-21 06:16:34.310Z | 303.537° NW | 2026-06-21 06:19:34.310Z | 249.916° W | 43.969° | 2026-06-21 06:23:34.310Z | 135.697° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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