KUIPER-00169, 65782
Orbit data source: Space-Track
KUIPER-00169, 65782 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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65782 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: 13 hours ago
TLE from 13 hours ago
0 KUIPER-00169
1 65782U 25217W 26171.30565473 .00002875 00000-0 40595-3 0 9993
2 65782 51.9027 299.3479 0000565 110.3787 249.7236 14.79938534 40213Epoch: 2026-06-20T07:20Z
TLE epoch observation values (Epoch: 2026-06-20T07:20:08.568Z)
Latitude
-0.00004°
Longitude
-79.21001°
Altitude
630.402 km
Speed
7.544 km/s
True Right ascension
19h 57m 23s
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
07:16:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.365 km
Perigee altitude
629.573 km
Semi-major axis
7,008.106 km
Eccentricity
0.00006
Inclination
51.9027°
RAAN
299.3479°
Arg. of periapsis
110.3787°
True anomaly
249.71753°
Mean anomaly
249.7236°
Eccentric anomaly
249.72056°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00040595
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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-00169 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 11:04:39.701Z | 218.638° SW | 2026-06-21 11:07:39.701Z | 108.977° ESE | 42.927° | 2026-06-21 11:11:39.701Z | 56.275° ENE |
| 6 mins | 2026-06-21 12:46:39.701Z | 289.733° WNW | 2026-06-21 12:49:39.701Z | 349.574° N | 25.462° | 2026-06-21 12:52:39.701Z | 35.07° NE |
| 4 mins | 2026-06-21 14:30:39.701Z | 340.14° N | 2026-06-21 14:31:39.701Z | 356.48° N | 17.133° | 2026-06-21 14:34:39.701Z | 39.86° NE |
| 6 mins | 2026-06-21 16:11:39.701Z | 330.981° NNW | 2026-06-21 16:14:39.701Z | 24.557° NE | 24.551° | 2026-06-21 16:17:39.701Z | 73.762° E |
| 7 mins | 2026-06-21 17:53:39.701Z | 304.182° NW | 2026-06-21 17:56:39.701Z | 169.447° S | 44.084° | 2026-06-21 18:00:39.701Z | 133.324° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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