KUIPER-00080, 64827
Orbit data source: Space-Track
KUIPER-00080, 64827 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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64827 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: 19 hours ago
TLE from 19 hours ago
0 KUIPER-00080
1 64827U 25151M 26166.37443889 -.00001004 00000-0 -10268-3 0 9995
2 64827 51.8998 228.6053 0000453 86.3101 273.7913 14.79924917 49778Epoch: 2026-06-15T08:59Z
TLE epoch observation values (Epoch: 2026-06-15T08:59:11.520Z)
Latitude
-0.00001°
Longitude
-169.85445°
Altitude
630.287 km
Speed
7.545 km/s
True Right ascension
15h 14m 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
14:43:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.33 km
Perigee altitude
629.695 km
Semi-major axis
7,008.149 km
Eccentricity
0.00005
Inclination
51.8998°
RAAN
228.6053°
Arg. of periapsis
86.3101°
True anomaly
273.78612°
Mean anomaly
273.7913°
Eccentric anomaly
273.78871°
Mean motion
3.69946 °/min
Orbital period
97.31 mins
BSTAR
-0.00010268
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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-00080 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 06:12:11.940Z | 201.108° SSW | 2026-06-16 06:16:11.940Z | 134.398° SE | 32.113° | 2026-06-16 06:20:11.940Z | 66.966° ENE |
| 6 mins | 2026-06-16 07:55:11.940Z | 272.99° WNW | 2026-06-16 07:57:11.940Z | 314.4° NW | 32.72° | 2026-06-16 08:01:11.940Z | 38.281° NE |
| 5 mins | 2026-06-16 09:38:11.940Z | 321.299° NNW | 2026-06-16 09:40:11.940Z | 353.685° N | 18.118° | 2026-06-16 09:43:11.940Z | 36.365° NE |
| 5 mins | 2026-06-16 11:21:11.940Z | 344.153° N | 2026-06-16 11:23:11.940Z | 20.025° NNE | 20.108° | 2026-06-16 11:26:11.940Z | 62.934° ENE |
| 7 mins | 2026-06-16 13:02:11.940Z | 318.788° NNW | 2026-06-16 13:05:11.940Z | 42.152° NE | 41.002° | 2026-06-16 13:09:11.940Z | 113.704° SE |
| 5 mins | 2026-06-16 14:44:11.940Z | 266.882° W | 2026-06-16 14:46:11.940Z | 231.32° WSW | 21.838° | 2026-06-16 14:49:11.940Z | 183.245° 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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