KUIPER-00136, 65962
Orbit data source: Space-Track
KUIPER-00136, 65962 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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65962 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00136
1 65962U 25228R 26170.61134316 .00002264 00000-0 32601-3 0 9997
2 65962 51.8999 257.4532 0000495 83.6062 276.4957 14.79921645 38494Epoch: 2026-06-19T14:40Z
TLE epoch observation values (Epoch: 2026-06-19T14:40:20.049Z)
Latitude
0.00003°
Longitude
129.53185°
Altitude
630.279 km
Speed
7.545 km/s
True Right ascension
17h 09m 48s
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
08:32:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.37 km
Perigee altitude
629.676 km
Semi-major axis
7,008.16 km
Eccentricity
0.00005
Inclination
51.8999°
RAAN
257.4532°
Arg. of periapsis
83.6062°
True anomaly
276.49006°
Mean anomaly
276.4957°
Eccentric anomaly
276.49288°
Mean motion
3.69945 °/min
Orbital period
97.31 mins
BSTAR
0.00032601
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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-00136 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 07:20:33.826Z | 187.678° SSW | 2026-06-21 07:23:33.826Z | 137.796° SSE | 26.801° | 2026-06-21 07:27:33.826Z | 72.118° E |
| 6 mins | 2026-06-21 09:02:33.826Z | 263.577° W | 2026-06-21 09:05:33.826Z | 349.397° N | 36.305° | 2026-06-21 09:08:33.826Z | 40.313° NE |
| 5 mins | 2026-06-21 10:45:33.826Z | 317.98° NNW | 2026-06-21 10:47:33.826Z | 351.509° N | 18.968° | 2026-06-21 10:50:33.826Z | 34.855° NE |
| 5 mins | 2026-06-21 12:28:33.826Z | 342.897° N | 2026-06-21 12:30:33.826Z | 17.36° NNE | 18.918° | 2026-06-21 12:33:33.826Z | 58.886° ENE |
| 7 mins | 2026-06-21 14:09:33.826Z | 322.439° NNW | 2026-06-21 14:12:33.826Z | 32.678° NE | 37.394° | 2026-06-21 14:16:33.826Z | 105.975° ESE |
| 6 mins | 2026-06-21 15:51:33.826Z | 273.884° WNW | 2026-06-21 15:53:33.826Z | 235.45° WSW | 26.429° | 2026-06-21 15:57:33.826Z | 169.136° S |
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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