KUIPER-00072, 64819
Orbit data source: Space-Track
KUIPER-00072, 64819 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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64819 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: 17 hours ago
TLE from 17 hours ago
0 KUIPER-00072
1 64819U 25151D 26166.42731795 .00001886 00000-0 27662-3 0 9990
2 64819 51.8964 210.8527 0000553 67.0340 293.0681 14.79887270 50020Epoch: 2026-06-15T10:15Z
TLE epoch observation values (Epoch: 2026-06-15T10:15:20.270Z)
Latitude
-0.00001°
Longitude
153.30438°
Altitude
630.274 km
Speed
7.545 km/s
True Right ascension
14h 03m 24s
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
13:37:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.519 km
Perigee altitude
629.744 km
Semi-major axis
7,008.269 km
Eccentricity
0.00006
Inclination
51.8964°
RAAN
210.8527°
Arg. of periapsis
67.034°
True anomaly
293.06227°
Mean anomaly
293.0681°
Eccentric anomaly
293.06518°
Mean motion
3.69936 °/min
Orbital period
97.31 mins
BSTAR
0.00027662
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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-00072 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-16 04:14:05.082Z | 155.611° SSE | 2026-06-16 04:16:05.082Z | 127.52° SE | 14.701° | 2026-06-16 04:18:05.082Z | 98.965° ESE |
| 7 mins | 2026-06-16 05:54:05.082Z | 232.926° WSW | 2026-06-16 05:57:05.082Z | 318.978° NNW | 44.963° | 2026-06-16 06:01:05.082Z | 51.685° ENE |
| 5 mins | 2026-06-16 07:37:05.082Z | 303.733° NW | 2026-06-16 07:39:05.082Z | 341.59° N | 23.129° | 2026-06-16 07:42:05.082Z | 30.915° NE |
| 4 mins | 2026-06-16 09:20:05.082Z | 335.802° NNW | 2026-06-16 09:22:05.082Z | 7.967° NNE | 17.2° | 2026-06-16 09:24:05.082Z | 37.654° NE |
| 6 mins | 2026-06-16 11:02:05.082Z | 336.329° NNW | 2026-06-16 11:04:05.082Z | 16.169° NNE | 27.613° | 2026-06-16 11:08:05.082Z | 85.456° E |
| 7 mins | 2026-06-16 12:43:05.082Z | 296.755° NW | 2026-06-16 12:46:05.082Z | 222.632° SW | 40.902° | 2026-06-16 12:50:05.082Z | 144.317° SSE |
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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