KUIPER-00115, 65152
Orbit data source: Space-Track
KUIPER-00115, 65152 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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65152 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-00115
1 65152U 25171W 26171.44703426 .00000326 00000-0 71743-4 0 9999
2 65152 51.9044 73.7027 0000757 97.2000 262.9049 14.79934517 47965Epoch: 2026-06-20T10:43Z
TLE epoch observation values (Epoch: 2026-06-20T10:43:43.760Z)
Latitude
0.00004°
Longitude
4.10887°
Altitude
630.344 km
Speed
7.544 km/s
True Right ascension
04h 54m 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
07:12:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.512 km
Perigee altitude
629.451 km
Semi-major axis
7,008.118 km
Eccentricity
0.00008
Inclination
51.9044°
RAAN
73.7027°
Arg. of periapsis
97.2°
True anomaly
262.89629°
Mean anomaly
262.9049°
Eccentric anomaly
262.9006°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.000071743
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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-00115 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-20 20:37:41.669Z | 234.899° WSW | 2026-06-20 20:41:41.669Z | 257.406° W | 43.133° | 2026-06-20 20:46:41.669Z | 50.835° ENE |
| 6 mins | 2026-06-20 22:21:41.669Z | 298.692° NW | 2026-06-20 22:24:41.669Z | 352.492° N | 22.083° | 2026-06-20 22:27:41.669Z | 35.325° NE |
| 4 mins | 2026-06-21 00:05:41.669Z | 343.433° N | 2026-06-21 00:06:41.669Z | 359.76° N | 17.308° | 2026-06-21 00:09:41.669Z | 43.962° NE |
| 6 mins | 2026-06-21 01:46:41.669Z | 330.118° NNW | 2026-06-21 01:49:41.669Z | 30.647° NE | 28.687° | 2026-06-21 01:52:41.669Z | 83.672° E |
| 6 mins | 2026-06-21 03:28:41.669Z | 291.079° WNW | 2026-06-21 03:30:41.669Z | 248.108° W | 38.368° | 2026-06-21 03:34:41.669Z | 148.907° SSE |
| 6 mins | 2026-06-21 19:18:41.669Z | 186.921° SSW | 2026-06-21 19:21:41.669Z | 119.995° SE | 29.614° | 2026-06-21 19:24:41.669Z | 71.821° E |
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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