KUIPER-00053, 64513
Orbit data source: Space-Track
KUIPER-00053, 64513 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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64513 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-00053
1 64513U 25134P 26170.59858054 .00001558 00000-0 22440-3 0 9998
2 64513 51.9002 131.6375 0000816 197.8530 162.2404 14.81644884 55313Epoch: 2026-06-19T14:21Z
TLE epoch observation values (Epoch: 2026-06-19T14:21:57.358Z)
Latitude
-0.00007°
Longitude
8.3232°
Altitude
625.428 km
Speed
7.547 km/s
True Right ascension
08h 46m 32s
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
07:17:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.16 km
Perigee altitude
624.017 km
Semi-major axis
7,002.725 km
Eccentricity
0.00008
Inclination
51.9002°
RAAN
131.6375°
Arg. of periapsis
197.853°
True anomaly
162.24325°
Mean anomaly
162.2404°
Eccentric anomaly
162.24183°
Mean motion
3.70376 °/min
Orbital period
97.2 mins
BSTAR
0.0002244
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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-00053 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 | 2026-06-20 22:53:40.196Z | 177.723° S | 2026-06-20 22:56:40.196Z | 127.337° SE | 22.723° | 2026-06-20 22:59:40.196Z | 80.239° E |
| 7 mins | 2026-06-21 00:34:40.196Z | 252.825° W | 2026-06-21 00:37:40.196Z | 330.143° NNW | 40.23° | 2026-06-21 00:41:40.196Z | 45.271° ENE |
| 5 mins | 2026-06-21 02:17:40.196Z | 312.025° NW | 2026-06-21 02:19:40.196Z | 345.763° N | 19.817° | 2026-06-21 02:22:40.196Z | 31.868° NE |
| 4 mins | 2026-06-21 04:00:40.196Z | 340.481° N | 2026-06-21 04:02:40.196Z | 13.847° NNE | 18.042° | 2026-06-21 04:04:40.196Z | 44.483° NE |
| 7 mins | 2026-06-21 05:41:40.196Z | 325.051° NNW | 2026-06-21 05:44:40.196Z | 29.569° NE | 34.026° | 2026-06-21 05:48:40.196Z | 99.813° ESE |
| 6 mins | 2026-06-21 07:23:40.196Z | 278.732° WNW | 2026-06-21 07:25:40.196Z | 236.04° WSW | 30.74° | 2026-06-21 07:29:40.196Z | 162.118° 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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