KUIPER-00110, 65148
Orbit data source: Space-Track
KUIPER-00110, 65148 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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65148 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-00110
1 65148U 25171S 26171.41328163 .00000844 00000-0 13970-3 0 9994
2 65148 51.8996 73.8911 0000824 105.1213 254.9840 14.79929759 47959Epoch: 2026-06-20T09:55Z
TLE epoch observation values (Epoch: 2026-06-20T09:55:07.532Z)
Latitude
-0.00008°
Longitude
16.48139°
Altitude
630.442 km
Speed
7.544 km/s
True Right ascension
04h 55m 33s
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
07:13:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.575 km
Perigee altitude
629.42 km
Semi-major axis
7,008.134 km
Eccentricity
0.00008
Inclination
51.8996°
RAAN
73.8911°
Arg. of periapsis
105.1213°
True anomaly
254.97488°
Mean anomaly
254.984°
Eccentric anomaly
254.97944°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.0001397
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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-00110 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 | 2026-06-20 21:29:31.707Z | 266.105° W | 2026-06-20 21:33:31.707Z | 347.186° N | 31.821° | 2026-06-20 21:36:31.707Z | 37.209° NE |
| 5 mins | 2026-06-20 23:13:31.707Z | 320.927° NNW | 2026-06-20 23:15:31.707Z | 352.638° N | 17.928° | 2026-06-20 23:18:31.707Z | 35.922° NE |
| 5 mins | 2026-06-21 00:56:31.707Z | 343.078° N | 2026-06-21 00:58:31.707Z | 19.002° NNE | 20.559° | 2026-06-21 01:01:31.707Z | 63.316° ENE |
| 7 mins | 2026-06-21 02:37:31.707Z | 317.085° NNW | 2026-06-21 02:40:31.707Z | 39.031° NE | 41.999° | 2026-06-21 02:44:31.707Z | 115.72° SE |
| 5 mins | 2026-06-21 04:19:31.707Z | 266.278° W | 2026-06-21 04:21:31.707Z | 232.262° WSW | 20.568° | 2026-06-21 04:24:31.707Z | 185.545° SSW |
| 7 mins | 2026-06-21 20:08:31.707Z | 229.476° WSW | 2026-06-21 20:11:31.707Z | 217.96° SW | 44.303° | 2026-06-21 20:15:31.707Z | 53.01° 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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