KUIPER-00070, 64817
Orbit data source: Space-Track
KUIPER-00070, 64817 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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64817 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: 23 hours ago
TLE from 23 hours ago
0 KUIPER-00070
1 64817U 25151B 26168.46242891 .00001986 00000-0 28952-3 0 9992
2 64817 51.8992 224.3613 0000516 81.6060 278.4960 14.79924992 51194Epoch: 2026-06-17T11:05Z
TLE epoch observation values (Epoch: 2026-06-17T11:05:53.857Z)
Latitude
-0.0001°
Longitude
152.16705°
Altitude
630.254 km
Speed
7.545 km/s
True Right ascension
14h 57m 26s
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
20:28:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.374 km
Perigee altitude
629.651 km
Semi-major axis
7,008.149 km
Eccentricity
0.00005
Inclination
51.8992°
RAAN
224.3613°
Arg. of periapsis
81.606°
True anomaly
278.49015°
Mean anomaly
278.496°
Eccentric anomaly
278.49308°
Mean motion
3.69946 °/min
Orbital period
97.31 mins
BSTAR
0.00028952
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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-00070 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 | 2026-06-18 10:10:15.192Z | 328.831° NNW | 2026-06-18 10:12:15.192Z | 358.526° N | 17.283° | 2026-06-18 10:15:15.192Z | 43.198° NE |
| 7 mins | 2026-06-18 11:52:15.192Z | 329.379° NNW | 2026-06-18 11:55:15.192Z | 28.583° NE | 28.761° | 2026-06-18 11:59:15.192Z | 90.202° ESE |
| 6 mins | 2026-06-18 13:34:15.192Z | 291.623° WNW | 2026-06-18 13:37:15.192Z | 197.813° SSW | 38.331° | 2026-06-18 13:40:15.192Z | 149.23° SSE |
| 6 mins | 2026-06-19 05:24:15.192Z | 187.697° SSW | 2026-06-19 05:27:15.192Z | 122.2° SE | 29.764° | 2026-06-19 05:30:15.192Z | 72.372° E |
| 7 mins | 2026-06-19 07:05:15.192Z | 264.787° W | 2026-06-19 07:08:15.192Z | 328.642° NNW | 34.811° | 2026-06-19 07:12:15.192Z | 41.453° NE |
| 4 mins | 2026-06-19 08:49:15.192Z | 326.644° NNW | 2026-06-19 08:50:15.192Z | 343.178° N | 18.214° | 2026-06-19 08:53:15.192Z | 30.092° 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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