KUIPER-00060, 64520
Orbit data source: Space-Track
KUIPER-00060, 64520 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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64520 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-00060
1 64520U 25134W 26171.32287705 .00009622 00000-0 12884-2 0 9997
2 64520 51.9022 126.7968 0000692 147.6526 212.4479 14.79963279 55438Epoch: 2026-06-20T07:44Z
TLE epoch observation values (Epoch: 2026-06-20T07:44:56.577Z)
Latitude
0°
Longitude
102.02191°
Altitude
630.596 km
Speed
7.544 km/s
True Right ascension
08h 27m 11s
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
07:12:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.376 km
Perigee altitude
629.406 km
Semi-major axis
7,008.028 km
Eccentricity
0.00007
Inclination
51.9022°
RAAN
126.7968°
Arg. of periapsis
147.6526°
True anomaly
212.44365°
Mean anomaly
212.4479°
Eccentric anomaly
212.44577°
Mean motion
3.69955 °/min
Orbital period
97.31 mins
BSTAR
0.0012884
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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-00060 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 22:29:18.416Z | 160.154° S | 2026-06-20 22:31:18.416Z | 130.351° SE | 16.904° | 2026-06-20 22:34:18.416Z | 87.58° E |
| 7 mins | 2026-06-21 00:09:18.416Z | 238.648° WSW | 2026-06-21 00:12:18.416Z | 295.276° NW | 44.093° | 2026-06-21 00:16:18.416Z | 49.262° ENE |
| 5 mins | 2026-06-21 01:52:18.416Z | 303.418° NW | 2026-06-21 01:54:18.416Z | 338.162° N | 21.96° | 2026-06-21 01:57:18.416Z | 28.687° NE |
| 5 mins | 2026-06-21 03:35:18.416Z | 333.822° NNW | 2026-06-21 03:37:18.416Z | 5.233° NNE | 17.462° | 2026-06-21 03:40:18.416Z | 47.613° ENE |
| 6 mins | 2026-06-21 05:17:18.416Z | 332.968° NNW | 2026-06-21 05:20:18.416Z | 40.127° NE | 28.894° | 2026-06-21 05:23:18.416Z | 87.598° E |
| 7 mins | 2026-06-21 06:58:18.416Z | 293.942° NW | 2026-06-21 07:01:18.416Z | 229.892° WSW | 38.154° | 2026-06-21 07:05:18.416Z | 149.701° SSE |
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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