KUIPER-00150, 65770
Orbit data source: Space-Track
KUIPER-00150, 65770 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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65770 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-00150
1 65770U 25217J 26171.42183622 .00002701 00000-0 38311-3 0 9996
2 65770 51.9020 316.3351 0000514 113.9416 246.1600 14.79935353 39988Epoch: 2026-06-20T10:07Z
TLE epoch observation values (Epoch: 2026-06-20T10:07:26.649Z)
Latitude
-0.00004°
Longitude
-104.16266°
Altitude
630.421 km
Speed
7.544 km/s
True Right ascension
21h 05m 20s
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
07:12:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.339 km
Perigee altitude
629.619 km
Semi-major axis
7,008.116 km
Eccentricity
0.00005
Inclination
51.902°
RAAN
316.3351°
Arg. of periapsis
113.9416°
True anomaly
246.15461°
Mean anomaly
246.16°
Eccentric anomaly
246.15731°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00038311
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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-00150 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 | 2026-06-20 20:24:01.775Z | 282.382° WNW | 2026-06-20 20:27:01.775Z | 236.009° WSW | 24.245° | 2026-06-20 20:31:01.775Z | 172.684° S |
| 7 mins | 2026-06-21 12:14:01.775Z | 221.53° SW | 2026-06-21 12:17:01.775Z | 184.587° SSW | 42.395° | 2026-06-21 12:21:01.775Z | 57.096° ENE |
| 6 mins | 2026-06-21 13:57:01.775Z | 293.292° NW | 2026-06-21 13:59:01.775Z | 331.366° NNW | 25.571° | 2026-06-21 14:03:01.775Z | 36.937° NE |
| 5 mins | 2026-06-21 15:40:01.775Z | 329.571° NNW | 2026-06-21 15:42:01.775Z | 0.83° NNE | 17.149° | 2026-06-21 15:45:01.775Z | 42.52° NE |
| 6 mins | 2026-06-21 17:22:01.775Z | 333.639° NNW | 2026-06-21 17:25:01.775Z | 30.55° NE | 24.498° | 2026-06-21 17:28:01.775Z | 76.39° E |
| 8 mins | 2026-06-21 19:03:01.775Z | 304.698° NW | 2026-06-21 19:06:01.775Z | 278.669° WNW | 43.144° | 2026-06-21 19:11:01.775Z | 133.836° SE |
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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