KUIPER-00058, 64518
Orbit data source: Space-Track
KUIPER-00058, 64518 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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64518 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: 14 hours ago
TLE from 14 hours ago
0 KUIPER-00058
1 64518U 25134U 26171.28372110 .00002310 00000-0 33187-3 0 9991
2 64518 51.8995 131.8707 0000724 70.5545 289.5496 14.79936728 55378Epoch: 2026-06-20T06:48Z
TLE epoch observation values (Epoch: 2026-06-20T06:48:33.503Z)
Latitude
0.00004°
Longitude
121.23057°
Altitude
630.101 km
Speed
7.545 km/s
True Right ascension
08h 47m 28s
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
07:15:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.482 km
Perigee altitude
629.468 km
Semi-major axis
7,008.112 km
Eccentricity
0.00007
Inclination
51.8995°
RAAN
131.8707°
Arg. of periapsis
70.5545°
True anomaly
289.54178°
Mean anomaly
289.5496°
Eccentric anomaly
289.54569°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00033187
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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-00058 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 23:09:53.789Z | 182.928° SSW | 2026-06-20 23:12:53.789Z | 135.348° SSE | 24.082° | 2026-06-20 23:16:53.789Z | 73.979° E |
| 7 mins | 2026-06-21 00:50:53.789Z | 252.763° W | 2026-06-21 00:53:53.789Z | 303.618° NW | 38.371° | 2026-06-21 00:57:53.789Z | 42.562° NE |
| 5 mins | 2026-06-21 02:34:53.789Z | 318.18° NNW | 2026-06-21 02:36:53.789Z | 353.206° N | 19.485° | 2026-06-21 02:39:53.789Z | 35.605° NE |
| 4 mins | 2026-06-21 04:17:53.789Z | 344.398° N | 2026-06-21 04:18:53.789Z | 0.864° NNE | 18.263° | 2026-06-21 04:21:53.789Z | 48.244° ENE |
| 7 mins | 2026-06-21 05:58:53.789Z | 325.235° NNW | 2026-06-21 06:01:53.789Z | 35.83° NE | 35.199° | 2026-06-21 06:05:53.789Z | 102.515° ESE |
| 6 mins | 2026-06-21 07:40:53.789Z | 276.247° WNW | 2026-06-21 07:42:53.789Z | 234.306° WSW | 29.317° | 2026-06-21 07:46:53.789Z | 164.41° 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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