KUIPER-00116, 65153
Orbit data source: Space-Track
KUIPER-00116, 65153 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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65153 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: 17 hours ago
TLE from 17 hours ago
0 KUIPER-00116
1 65153U 25171X 26171.13776846 .00003015 00000-0 42431-3 0 9991
2 65153 51.9006 80.1051 0000799 96.5761 263.5292 14.79939962 47848Epoch: 2026-06-20T03:18Z
TLE epoch observation values (Epoch: 2026-06-20T03:18:23.194Z)
Latitude
-0.00007°
Longitude
122.1517°
Altitude
630.324 km
Speed
7.544 km/s
True Right ascension
05h 20m 25s
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
07:14:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.525 km
Perigee altitude
629.405 km
Semi-major axis
7,008.102 km
Eccentricity
0.00008
Inclination
51.9006°
RAAN
80.1051°
Arg. of periapsis
96.5761°
True anomaly
263.5201°
Mean anomaly
263.5292°
Eccentric anomaly
263.52465°
Mean motion
3.6995 °/min
Orbital period
97.31 mins
BSTAR
0.00042431
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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-00116 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-20 21:19:31.248Z | 246.929° WSW | 2026-06-20 21:23:31.248Z | 298.7° NW | 39.193° | 2026-06-20 21:27:31.248Z | 43.347° NE |
| 5 mins | 2026-06-20 23:04:31.248Z | 317.027° NNW | 2026-06-20 23:06:31.248Z | 352.493° N | 19.823° | 2026-06-20 23:09:31.248Z | 35.22° NE |
| 4 mins | 2026-06-21 00:47:31.248Z | 343.859° N | 2026-06-21 00:48:31.248Z | 0.204° NNE | 18.035° | 2026-06-21 00:51:31.248Z | 47.205° ENE |
| 7 mins | 2026-06-21 02:28:31.248Z | 325.887° NNW | 2026-06-21 02:31:31.248Z | 33.77° NE | 34.179° | 2026-06-21 02:35:31.248Z | 100.487° ESE |
| 6 mins | 2026-06-21 04:10:31.248Z | 278.62° WNW | 2026-06-21 04:12:31.248Z | 236.305° WSW | 30.675° | 2026-06-21 04:16:31.248Z | 162.489° S |
| 7 mins | 2026-06-21 19:59:31.248Z | 208.966° SW | 2026-06-21 20:02:31.248Z | 157.052° SSE | 37.884° | 2026-06-21 20:06:31.248Z | 63.289° 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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