KUIPER-00093, 64838
Orbit data source: Space-Track
KUIPER-00093, 64838 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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64838 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00093
1 64838U 25151Y 26166.85524560 .00001135 00000-0 17787-3 0 9992
2 64838 51.8993 218.9906 0000437 106.4025 253.6985 14.79933653 49947Epoch: 2026-06-15T20:31Z
TLE epoch observation values (Epoch: 2026-06-15T20:31:33.219Z)
Latitude
-0.00007°
Longitude
6.96649°
Altitude
630.366 km
Speed
7.544 km/s
True Right ascension
14h 35m 57s
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
630.291 km
Perigee altitude
629.679 km
Semi-major axis
7,008.122 km
Eccentricity
0.00004
Inclination
51.8993°
RAAN
218.9906°
Arg. of periapsis
106.4025°
True anomaly
253.69369°
Mean anomaly
253.6985°
Eccentric anomaly
253.6961°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00017787
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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-00093 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-16 06:24:59.793Z | 228.176° WSW | 2026-06-16 06:29:59.793Z | 69.385° E | 43.366° | 2026-06-16 06:33:59.793Z | 53.573° ENE |
| 6 mins | 2026-06-16 08:08:59.793Z | 294.997° NW | 2026-06-16 08:10:59.793Z | 329.958° NNW | 23.907° | 2026-06-16 08:14:59.793Z | 35.695° NE |
| 5 mins | 2026-06-16 09:51:59.793Z | 328.876° NNW | 2026-06-16 09:53:59.793Z | 359.32° N | 17.17° | 2026-06-16 09:56:59.793Z | 42.455° NE |
| 6 mins | 2026-06-16 11:33:59.793Z | 331.582° NNW | 2026-06-16 11:36:59.793Z | 29.082° NE | 26.248° | 2026-06-16 11:39:59.793Z | 78.751° E |
| 7 mins | 2026-06-16 13:15:59.793Z | 298.137° NW | 2026-06-16 13:18:59.793Z | 181.721° SSW | 41.584° | 2026-06-16 13:22:59.793Z | 138.967° SSE |
| 6 mins | 2026-06-17 05:05:59.793Z | 180.316° SSW | 2026-06-17 05:08:59.793Z | 123.3° SE | 25.459° | 2026-06-17 05:11:59.793Z | 76.327° E |
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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