KUIPER-00089, 64834
Orbit data source: Space-Track
KUIPER-00089, 64834 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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64834 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: 8 hours ago
TLE from 8 hours ago
0 KUIPER-00089
1 64834U 25151U 26166.86333704 -.00000117 00000-0 13675-4 0 9990
2 64834 51.8990 211.4717 0000532 84.8151 275.2872 14.79929268 50059Epoch: 2026-06-15T20:43Z
TLE epoch observation values (Epoch: 2026-06-15T20:43:12.320Z)
Latitude
-0.00001°
Longitude
-3.47326°
Altitude
630.26 km
Speed
7.545 km/s
True Right ascension
14h 05m 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
14:52:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.372 km
Perigee altitude
629.626 km
Semi-major axis
7,008.136 km
Eccentricity
0.00005
Inclination
51.899°
RAAN
211.4717°
Arg. of periapsis
84.8151°
True anomaly
275.28113°
Mean anomaly
275.2872°
Eccentric anomaly
275.28416°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.000013675
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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-00089 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 | 2026-06-16 04:57:58.289Z | 190.365° SSW | 2026-06-16 05:01:58.289Z | 125.373° SE | 25.999° | 2026-06-16 05:04:58.289Z | 76.638° E |
| 7 mins | 2026-06-16 06:39:58.289Z | 258.328° W | 2026-06-16 06:42:58.289Z | 325.978° NNW | 37.746° | 2026-06-16 06:46:58.289Z | 43.118° NE |
| 5 mins | 2026-06-16 08:22:58.289Z | 311.075° NW | 2026-06-16 08:24:58.289Z | 342.145° N | 19.007° | 2026-06-16 08:27:58.289Z | 29.605° NE |
| 5 mins | 2026-06-16 10:05:58.289Z | 335.986° NNW | 2026-06-16 10:07:58.289Z | 8.032° NNE | 18.872° | 2026-06-16 10:10:58.289Z | 53.555° ENE |
| 6 mins | 2026-06-16 11:47:58.289Z | 327.117° NNW | 2026-06-16 11:49:58.289Z | 10.023° NNE | 35.89° | 2026-06-16 11:53:58.289Z | 102.435° ESE |
| 6 mins | 2026-06-16 13:28:58.289Z | 280.471° WNW | 2026-06-16 13:31:58.289Z | 222.796° SW | 27.304° | 2026-06-16 13:34:58.289Z | 171.83° 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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