KUIPER-00140, 65965
Orbit data source: Space-Track
KUIPER-00140, 65965 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 14 Oct 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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65965 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: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00140
1 65965U 25228U 26171.39065575 .00000405 00000-0 82123-4 0 9996
2 65965 51.8983 251.5229 0000539 91.5845 268.5179 14.79931668 38645Epoch: 2026-06-20T09:22Z
TLE epoch observation values (Epoch: 2026-06-20T09:22:32.656Z)
Latitude
-0.00004°
Longitude
-157.71916°
Altitude
630.296 km
Speed
7.544 km/s
True Right ascension
16h 46m 05s
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
07:14:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.369 km
Perigee altitude
629.614 km
Semi-major axis
7,008.128 km
Eccentricity
0.00005
Inclination
51.8983°
RAAN
251.5229°
Arg. of periapsis
91.5845°
True anomaly
268.51173°
Mean anomaly
268.5179°
Eccentric anomaly
268.51481°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.000082123
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Other satellites on launch #228 in the year 2025 (2025-10-14 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-00140 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 06:35:31.516Z | 159.34° S | 2026-06-21 06:37:31.516Z | 131.931° SE | 15.018° | 2026-06-21 06:40:31.516Z | 90.484° ESE |
| 7 mins | 2026-06-21 08:15:31.516Z | 233.863° WSW | 2026-06-21 08:18:31.516Z | 255.543° W | 44.358° | 2026-06-21 08:22:31.516Z | 51.067° ENE |
| 6 mins | 2026-06-21 09:58:31.516Z | 300.365° NW | 2026-06-21 10:00:31.516Z | 335.576° NNW | 22.79° | 2026-06-21 10:04:31.516Z | 37.103° NE |
| 5 mins | 2026-06-21 11:41:31.516Z | 332.165° NNW | 2026-06-21 11:43:31.516Z | 3.273° NNE | 17.311° | 2026-06-21 11:46:31.516Z | 45.714° ENE |
| 6 mins | 2026-06-21 13:23:31.516Z | 332.806° NNW | 2026-06-21 13:26:31.516Z | 35.928° NE | 27.715° | 2026-06-21 13:29:31.516Z | 84.041° E |
| 7 mins | 2026-06-21 15:04:31.516Z | 297.301° NW | 2026-06-21 15:07:31.516Z | 239.602° WSW | 40.053° | 2026-06-21 15:11:31.516Z | 146.085° 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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