KUIPER-00106, 65144
Orbit data source: Space-Track
KUIPER-00106, 65144 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 11 Aug 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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65144 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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00106
1 65144U 25171N 26171.36288071 .00015178 00000-0 20155-2 0 9995
2 65144 51.9013 50.3934 0000917 83.8883 276.2183 14.79930808 48291Epoch: 2026-06-20T08:42Z
TLE epoch observation values (Epoch: 2026-06-20T08:42:32.893Z)
Latitude
-0.00008°
Longitude
11.1777°
Altitude
630.22 km
Speed
7.545 km/s
True Right ascension
03h 21m 34s
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
07:15:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.636 km
Perigee altitude
629.351 km
Semi-major axis
7,008.131 km
Eccentricity
0.00009
Inclination
51.9013°
RAAN
50.3934°
Arg. of periapsis
83.8883°
True anomaly
276.20785°
Mean anomaly
276.2183°
Eccentric anomaly
276.21308°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.0020155
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Other satellites on launch #171 in the year 2025 (2025-08-11 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-00106 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 | 2026-06-20 20:19:54.961Z | 298.844° NW | 2026-06-20 20:21:54.961Z | 345.911° N | 27.077° | 2026-06-20 20:24:54.961Z | 34.448° NE |
| 4 mins | 2026-06-20 22:02:54.961Z | 337.295° NNW | 2026-06-20 22:03:54.961Z | 353.557° N | 17.177° | 2026-06-20 22:06:54.961Z | 37.538° NE |
| 5 mins | 2026-06-20 23:44:54.961Z | 342.021° N | 2026-06-20 23:46:54.961Z | 20.493° NNE | 23.398° | 2026-06-20 23:49:54.961Z | 69.751° E |
| 7 mins | 2026-06-21 01:25:54.961Z | 308.021° NW | 2026-06-21 01:28:54.961Z | 122.925° SE | 44.926° | 2026-06-21 01:32:54.961Z | 128.82° SE |
| 5 mins | 2026-06-21 17:16:54.961Z | 164.209° S | 2026-06-21 17:18:54.961Z | 131.412° SE | 19.733° | 2026-06-21 17:21:54.961Z | 85.234° E |
| 7 mins | 2026-06-21 18:56:54.961Z | 245.092° WSW | 2026-06-21 18:59:54.961Z | 304.01° NW | 42.273° | 2026-06-21 19:03:54.961Z | 46.57° ENE |
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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