KUIPER-00094, 64839
Orbit data source: Space-Track
KUIPER-00094, 64839 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Wed, 16 Jul 2025 UTC via an FALCON 9 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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64839 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-00094
1 64839U 25151Z 26166.22833736 .00001587 00000-0 23867-3 0 9999
2 64839 51.9022 176.8391 0002412 25.9405 334.1678 14.79653906 50489Epoch: 2026-06-15T05:28Z
TLE epoch observation values (Epoch: 2026-06-15T05:28:48.347Z)
Latitude
-0.00002°
Longitude
-168.8801°
Altitude
629.642 km
Speed
7.546 km/s
True Right ascension
11h 47m 21s
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
15:50:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.558 km
Perigee altitude
629.177 km
Semi-major axis
7,009.005 km
Eccentricity
0.00024
Inclination
51.9022°
RAAN
176.8391°
Arg. of periapsis
25.9405°
True anomaly
334.15575°
Mean anomaly
334.1678°
Eccentric anomaly
334.16178°
Mean motion
3.69878 °/min
Orbital period
97.33 mins
BSTAR
0.00023867
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Other satellites on launch #151 in the year 2025 (2025-07-16 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-00094 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 | 2026-06-16 06:06:59.910Z | 309.791° NW | 2026-06-16 06:09:59.910Z | 355.175° N | 18.283° | 2026-06-16 06:12:59.910Z | 37.022° NE |
| 5 mins | 2026-06-16 07:50:59.910Z | 345.316° N | 2026-06-16 07:52:59.910Z | 21.115° NNE | 19.674° | 2026-06-16 07:55:59.910Z | 62.633° ENE |
| 7 mins | 2026-06-16 09:31:59.910Z | 320.407° NNW | 2026-06-16 09:34:59.910Z | 43.707° NE | 39.967° | 2026-06-16 09:38:59.910Z | 111.785° ESE |
| 5 mins | 2026-06-16 11:13:59.910Z | 267.911° W | 2026-06-16 11:15:59.910Z | 230.963° WSW | 23.136° | 2026-06-16 11:18:59.910Z | 181.232° SSW |
| 7 mins | 2026-06-17 03:02:59.910Z | 224.287° SW | 2026-06-17 03:05:59.910Z | 193.389° SSW | 43.154° | 2026-06-17 03:09:59.910Z | 55.62° ENE |
| 6 mins | 2026-06-17 04:45:59.910Z | 294.6° NW | 2026-06-17 04:47:59.910Z | 331.626° NNW | 24.837° | 2026-06-17 04:51:59.910Z | 36.666° NE |
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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