KUIPER-00146, 65967
Orbit data source: Space-Track
KUIPER-00146, 65967 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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65967 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: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00146
1 65967U 25228W 26171.42712752 .00000905 00000-0 14769-3 0 9993
2 65967 51.9022 248.9191 0000761 110.0084 250.0960 14.79930239 38680Epoch: 2026-06-20T10:15Z
TLE epoch observation values (Epoch: 2026-06-20T10:15:03.817Z)
Latitude
-0.00006°
Longitude
-173.48876°
Altitude
630.473 km
Speed
7.544 km/s
True Right ascension
16h 35m 40s
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
07:14:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.528 km
Perigee altitude
629.462 km
Semi-major axis
7,008.132 km
Eccentricity
0.00008
Inclination
51.9022°
RAAN
248.9191°
Arg. of periapsis
110.0084°
True anomaly
250.0878°
Mean anomaly
250.096°
Eccentric anomaly
250.0919°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00014769
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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-00146 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 07:29:09.046Z | 208.043° SW | 2026-06-21 07:32:09.046Z | 159.31° S | 36.904° | 2026-06-21 07:36:09.046Z | 64.351° ENE |
| 7 mins | 2026-06-21 09:11:09.046Z | 275.189° WNW | 2026-06-21 09:14:09.046Z | 331.256° NNW | 29.683° | 2026-06-21 09:18:09.046Z | 38.975° NE |
| 4 mins | 2026-06-21 10:55:09.046Z | 328.903° NNW | 2026-06-21 10:57:09.046Z | 1.524° NNE | 17.35° | 2026-06-21 10:59:09.046Z | 31.04° NE |
| 6 mins | 2026-06-21 12:37:09.046Z | 335.843° NNW | 2026-06-21 12:39:09.046Z | 9.193° NNE | 21.706° | 2026-06-21 12:43:09.046Z | 70.695° E |
| 7 mins | 2026-06-21 14:18:09.046Z | 311.641° NW | 2026-06-21 14:21:09.046Z | 345.158° N | 42.967° | 2026-06-21 14:25:09.046Z | 121.508° SE |
| 4 mins | 2026-06-21 16:01:09.046Z | 255.784° W | 2026-06-21 16:02:09.046Z | 240.07° WSW | 16.945° | 2026-06-21 16:05:09.046Z | 195.12° 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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