KUIPER-00096, 65135
Orbit data source: Space-Track
KUIPER-00096, 65135 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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65135 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-00096
1 65135U 25171D 26171.39028750 .00001801 00000-0 26515-3 0 9999
2 65135 51.8987 63.9319 0000698 108.2950 251.8088 14.79936978 48107Epoch: 2026-06-20T09:22Z
TLE epoch observation values (Epoch: 2026-06-20T09:22:00.840Z)
Latitude
-0.00007°
Longitude
14.82275°
Altitude
630.422 km
Speed
7.544 km/s
True Right ascension
04h 15m 43s
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
07:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.464 km
Perigee altitude
629.485 km
Semi-major axis
7,008.111 km
Eccentricity
0.00007
Inclination
51.8987°
RAAN
63.9319°
Arg. of periapsis
108.295°
True anomaly
251.8012°
Mean anomaly
251.8088°
Eccentric anomaly
251.805°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00026515
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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-00096 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 20:56:54.717Z | 270.783° WNW | 2026-06-20 20:59:54.717Z | 321.611° NNW | 30.348° | 2026-06-20 21:03:54.717Z | 37.565° NE |
| 5 mins | 2026-06-20 22:40:54.717Z | 324.377° NNW | 2026-06-20 22:42:54.717Z | 356.31° N | 17.628° | 2026-06-20 22:45:54.717Z | 38.291° NE |
| 5 mins | 2026-06-21 00:23:54.717Z | 345.786° N | 2026-06-21 00:25:54.717Z | 23.413° NE | 21.216° | 2026-06-21 00:28:54.717Z | 66.963° ENE |
| 7 mins | 2026-06-21 02:04:54.717Z | 315.191° NNW | 2026-06-21 02:07:54.717Z | 64° ENE | 43.053° | 2026-06-21 02:11:54.717Z | 120.081° SE |
| 5 mins | 2026-06-21 03:46:54.717Z | 261.231° W | 2026-06-21 03:48:54.717Z | 228.163° WSW | 18.39° | 2026-06-21 03:51:54.717Z | 186.466° SSW |
| 7 mins | 2026-06-21 19:35:54.717Z | 234.614° WSW | 2026-06-21 19:38:54.717Z | 291.471° WNW | 44.8° | 2026-06-21 19:42:54.717Z | 50.975° 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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