KUIPER-00071, 64818
Orbit data source: Space-Track
KUIPER-00071, 64818 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Wed, 16 Jul 2025 UTC via an FALCON 9 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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64818 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00071
1 64818U 25151C 26168.39783748 .00002080 00000-0 30204-3 0 9995
2 64818 51.9005 222.1852 0000166 88.1526 271.9455 14.79881536 50037Epoch: 2026-06-17T09:32Z
TLE epoch observation values (Epoch: 2026-06-17T09:32:53.158Z)
Latitude
-0.00004°
Longitude
173.30758°
Altitude
630.441 km
Speed
7.544 km/s
True Right ascension
14h 48m 44s
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
20:27:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.266 km
Perigee altitude
630.033 km
Semi-major axis
7,008.286 km
Eccentricity
0.00002
Inclination
51.9005°
RAAN
222.1852°
Arg. of periapsis
88.1526°
True anomaly
271.9436°
Mean anomaly
271.9455°
Eccentric anomaly
271.94455°
Mean motion
3.69935 °/min
Orbital period
97.31 mins
BSTAR
0.00030204
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Other satellites on launch #151 in the year 2025 (2025-07-16 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-00071 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-18 10:14:24.910Z | 321.711° NNW | 2026-06-18 10:17:24.910Z | 3.092° NNE | 17.86° | 2026-06-18 10:20:24.910Z | 47.908° ENE |
| 6 mins | 2026-06-18 11:57:24.910Z | 329.105° NNW | 2026-06-18 12:00:24.910Z | 38.287° NE | 32.012° | 2026-06-18 12:03:24.910Z | 91.901° ESE |
| 7 mins | 2026-06-18 13:38:24.910Z | 289.871° WNW | 2026-06-18 13:41:24.910Z | 232.947° WSW | 33.721° | 2026-06-18 13:45:24.910Z | 157.298° SSE |
| 7 mins | 2026-06-19 05:28:24.910Z | 203.431° SW | 2026-06-19 05:31:24.910Z | 148.849° SSE | 35.477° | 2026-06-19 05:35:24.910Z | 65.474° ENE |
| 7 mins | 2026-06-19 07:10:24.910Z | 274.351° WNW | 2026-06-19 07:13:24.910Z | 336.943° NNW | 30.965° | 2026-06-19 07:17:24.910Z | 40.665° NE |
| 4 mins | 2026-06-19 08:54:24.910Z | 331.2° NNW | 2026-06-19 08:55:24.910Z | 347.423° N | 17.543° | 2026-06-19 08:58:24.910Z | 32.944° NE |
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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