KUIPER-00086, 64832
Orbit data source: Space-Track
KUIPER-00086, 64832 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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64832 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: 8 hours ago
TLE from 8 hours ago
0 KUIPER-00086
1 64832U 25151S 26166.84982974 .00002170 00000-0 31359-3 0 9993
2 64832 51.8998 224.0451 0000527 96.0271 264.0751 14.79929006 49872Epoch: 2026-06-15T20:23Z
TLE epoch observation values (Epoch: 2026-06-15T20:23:45.289Z)
Latitude
-0.00005°
Longitude
13.97605°
Altitude
630.333 km
Speed
7.544 km/s
True Right ascension
14h 56m 10s
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
14:52:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.369 km
Perigee altitude
629.63 km
Semi-major axis
7,008.136 km
Eccentricity
0.00005
Inclination
51.8998°
RAAN
224.0451°
Arg. of periapsis
96.0271°
True anomaly
264.06909°
Mean anomaly
264.0751°
Eccentric anomaly
264.0721°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00031359
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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-00086 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-16 06:16:58.307Z | 208.143° SW | 2026-06-16 06:20:58.307Z | 118.121° SE | 36.996° | 2026-06-16 06:24:58.307Z | 61.32° ENE |
| 6 mins | 2026-06-16 07:59:58.307Z | 284.008° WNW | 2026-06-16 08:01:58.307Z | 327.131° NNW | 29.768° | 2026-06-16 08:05:58.307Z | 38.213° NE |
| 4 mins | 2026-06-16 09:42:58.307Z | 326.938° NNW | 2026-06-16 09:44:58.307Z | 359.19° N | 17.462° | 2026-06-16 09:46:58.307Z | 29.382° NE |
| 6 mins | 2026-06-16 11:24:58.307Z | 334.249° NNW | 2026-06-16 11:27:58.307Z | 26.949° NE | 21.482° | 2026-06-16 11:30:58.307Z | 69.346° E |
| 7 mins | 2026-06-16 13:06:58.307Z | 314.15° NW | 2026-06-16 13:09:58.307Z | 84.868° E | 42.932° | 2026-06-16 13:13:58.307Z | 122.303° SE |
| 4 mins | 2026-06-16 14:48:58.307Z | 257.944° W | 2026-06-16 14:50:58.307Z | 225.406° WSW | 17.229° | 2026-06-16 14:52:58.307Z | 196.369° SSW |
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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