KUIPER-00049, 64509
Orbit data source: Space-Track
KUIPER-00049, 64509 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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64509 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-00049
1 64509U 25134K 26171.31479410 .00002340 00000-0 33587-3 0 9993
2 64509 51.8994 134.2247 0000706 63.3482 296.7552 14.79931772 55347Epoch: 2026-06-20T07:33Z
TLE epoch observation values (Epoch: 2026-06-20T07:33:18.210Z)
Latitude
-0.00005°
Longitude
112.36759°
Altitude
630.063 km
Speed
7.545 km/s
True Right ascension
08h 56m 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
07:15:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.486 km
Perigee altitude
629.496 km
Semi-major axis
7,008.128 km
Eccentricity
0.00007
Inclination
51.8994°
RAAN
134.2247°
Arg. of periapsis
63.3482°
True anomaly
296.74798°
Mean anomaly
296.7552°
Eccentric anomaly
296.75159°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00033587
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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-00049 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 23:55:38.812Z | 208.505° SW | 2026-06-20 23:59:38.812Z | 112.736° SE | 37.038° | 2026-06-21 00:02:38.812Z | 64.328° ENE |
| 7 mins | 2026-06-21 01:37:38.812Z | 275.116° WNW | 2026-06-21 01:40:38.812Z | 330.334° NNW | 29.557° | 2026-06-21 01:44:38.812Z | 38.733° NE |
| 4 mins | 2026-06-21 03:21:38.812Z | 328.487° NNW | 2026-06-21 03:23:38.812Z | 0.985° NNE | 17.368° | 2026-06-21 03:25:38.812Z | 30.688° NE |
| 6 mins | 2026-06-21 05:03:38.812Z | 335.42° NNW | 2026-06-21 05:05:38.812Z | 8.534° NNE | 21.735° | 2026-06-21 05:09:38.812Z | 70.58° E |
| 8 mins | 2026-06-21 06:44:38.812Z | 311.414° NW | 2026-06-21 06:47:38.812Z | 342.086° N | 42.861° | 2026-06-21 06:52:38.812Z | 123.145° SE |
| 4 mins | 2026-06-21 08:27:38.812Z | 256.107° W | 2026-06-21 08:28:38.812Z | 240.534° WSW | 16.789° | 2026-06-21 08:31:38.812Z | 195.642° SSW |
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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