KUIPER-00046, 64506
Orbit data source: Space-Track
KUIPER-00046, 64506 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 23 Jun 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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64506 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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00046
1 64506U 25134G 26171.33237933 .00001985 00000-0 28932-3 0 9996
2 64506 51.8973 149.1494 0000626 73.2855 286.8176 14.79925374 55135Epoch: 2026-06-20T07:58Z
TLE epoch observation values (Epoch: 2026-06-20T07:58:37.574Z)
Latitude
-0°
Longitude
120.94432°
Altitude
630.179 km
Speed
7.545 km/s
True Right ascension
09h 56m 35s
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
07:15:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.45 km
Perigee altitude
629.573 km
Semi-major axis
7,008.148 km
Eccentricity
0.00006
Inclination
51.8973°
RAAN
149.1494°
Arg. of periapsis
73.2855°
True anomaly
286.81073°
Mean anomaly
286.8176°
Eccentric anomaly
286.81417°
Mean motion
3.69946 °/min
Orbital period
97.31 mins
BSTAR
0.00028932
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Other satellites on launch #134 in the year 2025 (2025-06-23 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-00046 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 | 2026-06-21 00:20:09.802Z | 182.265° SSW | 2026-06-21 00:23:09.802Z | 132.097° SE | 24.569° | 2026-06-21 00:26:09.802Z | 80.589° E |
| 7 mins | 2026-06-21 02:01:09.802Z | 254.168° W | 2026-06-21 02:04:09.802Z | 311.288° NW | 38.529° | 2026-06-21 02:08:09.802Z | 42.9° NE |
| 5 mins | 2026-06-21 03:45:09.802Z | 320.403° NNW | 2026-06-21 03:47:09.802Z | 355.765° N | 19.281° | 2026-06-21 03:50:09.802Z | 36.861° NE |
| 4 mins | 2026-06-21 05:28:09.802Z | 346.472° N | 2026-06-21 05:29:09.802Z | 3.299° NNE | 18.46° | 2026-06-21 05:32:09.802Z | 49.992° ENE |
| 7 mins | 2026-06-21 07:09:09.802Z | 326.052° NNW | 2026-06-21 07:12:09.802Z | 41.677° NE | 35.325° | 2026-06-21 07:16:09.802Z | 103.692° ESE |
| 6 mins | 2026-06-21 08:51:09.802Z | 273.87° WNW | 2026-06-21 08:53:09.802Z | 230.189° WSW | 28.984° | 2026-06-21 08:57:09.802Z | 164.241° 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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