KUIPER-00097, 65136
Orbit data source: Space-Track
KUIPER-00097, 65136 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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65136 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-00097
1 65136U 25171E 26170.91490725 -.00000275 00000-0 -70789-5 0 9992
2 65136 51.9010 68.6851 0000917 99.0222 261.0844 14.79931122 47986Epoch: 2026-06-19T21:57Z
TLE epoch observation values (Epoch: 2026-06-19T21:57:27.986Z)
Latitude
-0.00003°
Longitude
-168.81857°
Altitude
630.388 km
Speed
7.544 km/s
True Right ascension
04h 34m 44s
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
08:32:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.635 km
Perigee altitude
629.35 km
Semi-major axis
7,008.13 km
Eccentricity
0.00009
Inclination
51.901°
RAAN
68.6851°
Arg. of periapsis
99.0222°
True anomaly
261.07402°
Mean anomaly
261.0844°
Eccentric anomaly
261.07921°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
-0.0000070789
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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-00097 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 22:35:02.233Z | 306.344° NW | 2026-06-20 22:38:02.233Z | 349.261° N | 18.348° | 2026-06-20 22:41:02.233Z | 33.774° NE |
| 5 mins | 2026-06-21 00:19:02.233Z | 340.796° N | 2026-06-21 00:21:02.233Z | 15.22° NNE | 19.797° | 2026-06-21 00:24:02.233Z | 59.663° ENE |
| 7 mins | 2026-06-21 02:00:02.233Z | 318.919° NNW | 2026-06-21 02:03:02.233Z | 25.641° NE | 39.87° | 2026-06-21 02:07:02.233Z | 110.51° ESE |
| 6 mins | 2026-06-21 03:42:02.233Z | 271.641° WNW | 2026-06-21 03:44:02.233Z | 236.945° WSW | 23.104° | 2026-06-21 03:48:02.233Z | 174.708° S |
| 8 mins | 2026-06-21 19:31:02.233Z | 223.873° SW | 2026-06-21 19:35:02.233Z | 85.413° E | 42.751° | 2026-06-21 19:39:02.233Z | 54.932° ENE |
| 6 mins | 2026-06-21 21:14:02.233Z | 293.456° NW | 2026-06-21 21:16:02.233Z | 329.919° NNW | 24.896° | 2026-06-21 21:20:02.233Z | 36.19° NE |
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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