KUIPER-00047, 64507
Orbit data source: Space-Track
KUIPER-00047, 64507 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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64507 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00047
1 64507U 25134H 26170.58544686 .00000138 00000-0 47125-4 0 9994
2 64507 51.8997 124.9737 0000645 87.6609 272.4427 14.79932084 55406Epoch: 2026-06-19T14:03Z
TLE epoch observation values (Epoch: 2026-06-19T14:03:02.608Z)
Latitude
-0.00005°
Longitude
6.40049°
Altitude
630.266 km
Speed
7.545 km/s
True Right ascension
08h 19m 53s
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
07:15:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.442 km
Perigee altitude
629.538 km
Semi-major axis
7,008.127 km
Eccentricity
0.00006
Inclination
51.8997°
RAAN
124.9737°
Arg. of periapsis
87.6609°
True anomaly
272.43532°
Mean anomaly
272.4427°
Eccentric anomaly
272.43901°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.000047125
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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-00047 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 22:37:02.790Z | 186.758° SSW | 2026-06-20 22:40:02.790Z | 136.665° SSE | 26.448° | 2026-06-20 22:44:02.790Z | 72.18° E |
| 6 mins | 2026-06-21 00:19:02.790Z | 263.274° W | 2026-06-21 00:21:02.790Z | 305.561° NW | 36.404° | 2026-06-21 00:25:02.790Z | 40.78° NE |
| 5 mins | 2026-06-21 02:02:02.790Z | 318.432° NNW | 2026-06-21 02:04:02.790Z | 352.296° N | 19.023° | 2026-06-21 02:07:02.790Z | 35.248° NE |
| 4 mins | 2026-06-21 03:45:02.790Z | 343.556° N | 2026-06-21 03:47:02.790Z | 18.111° NNE | 18.792° | 2026-06-21 03:49:02.790Z | 48.753° ENE |
| 7 mins | 2026-06-21 05:26:02.790Z | 323.043° NNW | 2026-06-21 05:29:02.790Z | 34.647° NE | 37.082° | 2026-06-21 05:33:02.790Z | 105.615° ESE |
| 6 mins | 2026-06-21 07:08:02.790Z | 273.792° WNW | 2026-06-21 07:10:02.790Z | 234.503° WSW | 26.847° | 2026-06-21 07:14:02.790Z | 168.292° 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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