KUIPER-00156, 65775
Orbit data source: Space-Track
KUIPER-00156, 65775 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 25 Sep 2025 UTC via an ATLAS V 551 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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65775 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00156
1 65775U 25217P 26170.63845493 .00001611 00000-0 24032-3 0 9998
2 65775 51.9025 294.8355 0000614 107.6228 252.4802 14.79931074 40212Epoch: 2026-06-19T15:19Z
TLE epoch observation values (Epoch: 2026-06-19T15:19:22.505Z)
Latitude
-0°
Longitude
157.12717°
Altitude
630.418 km
Speed
7.544 km/s
True Right ascension
19h 39m 20s
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
07:13:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.423 km
Perigee altitude
629.562 km
Semi-major axis
7,008.129 km
Eccentricity
0.00006
Inclination
51.9025°
RAAN
294.8355°
Arg. of periapsis
107.6228°
True anomaly
252.47349°
Mean anomaly
252.4802°
Eccentric anomaly
252.47685°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00024032
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Other satellites on launch #217 in the year 2025 (2025-09-25 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-00156 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 09:36:49.220Z | 176.852° S | 2026-06-21 09:39:49.220Z | 126.417° SE | 22.577° | 2026-06-21 09:42:49.220Z | 80.118° E |
| 7 mins | 2026-06-21 11:17:49.220Z | 251.987° W | 2026-06-21 11:20:49.220Z | 325.226° NNW | 40.47° | 2026-06-21 11:24:49.220Z | 45.147° ENE |
| 5 mins | 2026-06-21 13:00:49.220Z | 309.393° NW | 2026-06-21 13:02:49.220Z | 341.984° N | 19.932° | 2026-06-21 13:05:49.220Z | 29.781° NE |
| 5 mins | 2026-06-21 14:43:49.220Z | 336.152° NNW | 2026-06-21 14:45:49.220Z | 8.143° NNE | 18.245° | 2026-06-21 14:48:49.220Z | 51.893° ENE |
| 6 mins | 2026-06-21 16:25:49.220Z | 330.361° NNW | 2026-06-21 16:27:49.220Z | 13.081° NNE | 33.411° | 2026-06-21 16:31:49.220Z | 97.198° ESE |
| 7 mins | 2026-06-21 18:06:49.220Z | 284.662° WNW | 2026-06-21 18:09:49.220Z | 222.117° SW | 31.158° | 2026-06-21 18:13:49.220Z | 159.637° S |
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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