KUIPER-00152, 65772
Orbit data source: Space-Track
KUIPER-00152, 65772 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 25 Sep 2025 UTC via an ATLAS V 551 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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65772 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: 13 hours ago
TLE from 13 hours ago
0 KUIPER-00152
1 65772U 25217L 26171.34211308 .00001135 00000-0 17794-3 0 9994
2 65772 51.9002 296.6725 0000631 105.2675 254.8357 14.79929595 40254Epoch: 2026-06-20T08:12Z
TLE epoch observation values (Epoch: 2026-06-20T08:12:38.570Z)
Latitude
-0.00001°
Longitude
-95.04633°
Altitude
630.409 km
Speed
7.544 km/s
True Right ascension
19h 46m 41s
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
08:32:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.44 km
Perigee altitude
629.555 km
Semi-major axis
7,008.135 km
Eccentricity
0.00006
Inclination
51.9002°
RAAN
296.6725°
Arg. of periapsis
105.2675°
True anomaly
254.82872°
Mean anomaly
254.8357°
Eccentric anomaly
254.83221°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00017794
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Other satellites on launch #217 in the year 2025 (2025-09-25 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-00152 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 10:17:39.159Z | 196.888° SSW | 2026-06-21 10:21:39.159Z | 121.487° SE | 30.439° | 2026-06-21 10:24:39.159Z | 71.608° E |
| 7 mins | 2026-06-21 11:59:39.159Z | 265.871° W | 2026-06-21 12:02:39.159Z | 329.025° NNW | 34.3° | 2026-06-21 12:06:39.159Z | 41.189° NE |
| 4 mins | 2026-06-21 13:43:39.159Z | 326.918° NNW | 2026-06-21 13:44:39.159Z | 343.348° N | 18.087° | 2026-06-21 13:47:39.159Z | 30.188° NE |
| 5 mins | 2026-06-21 15:25:39.159Z | 336.308° NNW | 2026-06-21 15:27:39.159Z | 8.852° NNE | 19.851° | 2026-06-21 15:30:39.159Z | 56.489° ENE |
| 7 mins | 2026-06-21 17:06:39.159Z | 317.016° NNW | 2026-06-21 17:09:39.159Z | 6.19° NNE | 39.189° | 2026-06-21 17:13:39.159Z | 109.85° ESE |
| 6 mins | 2026-06-21 18:48:39.159Z | 275.092° WNW | 2026-06-21 18:51:39.159Z | 222.404° SW | 22.741° | 2026-06-21 18:54:39.159Z | 177.879° 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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