KUIPER-00079, 64826
Orbit data source: Space-Track
KUIPER-00079, 64826 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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64826 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: 7 hours ago
TLE from 7 hours ago
0 KUIPER-00079
1 64826U 25151L 26166.88091671 .00000984 00000-0 15806-3 0 9995
2 64826 51.8989 226.3562 0000531 93.7337 266.3687 14.79932030 51041Epoch: 2026-06-15T21:08Z
TLE epoch observation values (Epoch: 2026-06-15T21:08:31.203Z)
Latitude
0.00004°
Longitude
5.06527°
Altitude
630.309 km
Speed
7.544 km/s
True Right ascension
15h 05m 25s
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
14:43:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.362 km
Perigee altitude
629.618 km
Semi-major axis
7,008.127 km
Eccentricity
0.00005
Inclination
51.8989°
RAAN
226.3562°
Arg. of periapsis
93.7337°
True anomaly
266.36263°
Mean anomaly
266.3687°
Eccentric anomaly
266.36566°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00015806
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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-00079 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 05:23:33.094Z | 158.805° S | 2026-06-16 05:25:33.094Z | 131.505° SE | 14.814° | 2026-06-16 05:27:33.094Z | 102.028° ESE |
| 7 mins | 2026-06-16 07:03:33.094Z | 233.31° WSW | 2026-06-16 07:06:33.094Z | 252.674° W | 44.486° | 2026-06-16 07:10:33.094Z | 51.329° ENE |
| 6 mins | 2026-06-16 08:46:33.094Z | 300.492° NW | 2026-06-16 08:48:33.094Z | 336.104° NNW | 22.928° | 2026-06-16 08:52:33.094Z | 37.328° NE |
| 5 mins | 2026-06-16 10:29:33.094Z | 332.479° NNW | 2026-06-16 10:31:33.094Z | 3.717° NNE | 17.292° | 2026-06-16 10:34:33.094Z | 45.877° ENE |
| 6 mins | 2026-06-16 12:11:33.094Z | 333.238° NNW | 2026-06-16 12:14:33.094Z | 36.503° NE | 27.49° | 2026-06-16 12:17:33.094Z | 83.92° E |
| 7 mins | 2026-06-16 13:52:33.094Z | 297.532° NW | 2026-06-16 13:55:33.094Z | 238.573° WSW | 40.366° | 2026-06-16 13:59:33.094Z | 145.483° 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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