KUIPER-00090, 64835
Orbit data source: Space-Track
KUIPER-00090, 64835 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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64835 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: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00090
1 64835U 25151V 26166.80389059 .00001792 00000-0 26393-3 0 9998
2 64835 51.8964 204.2456 0000480 83.5438 276.5579 14.79937044 50146Epoch: 2026-06-15T19:17Z
TLE epoch observation values (Epoch: 2026-06-15T19:17:36.146Z)
Latitude
-0.00004°
Longitude
10.75993°
Altitude
630.231 km
Speed
7.545 km/s
True Right ascension
13h 36m 58s
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
15:50:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.311 km
Perigee altitude
629.638 km
Semi-major axis
7,008.112 km
Eccentricity
0.00005
Inclination
51.8964°
RAAN
204.2456°
Arg. of periapsis
83.5438°
True anomaly
276.55244°
Mean anomaly
276.5579°
Eccentric anomaly
276.55517°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00026393
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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-00090 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 05:13:08.232Z | 207.158° SW | 2026-06-16 05:15:08.232Z | 122.799° SE | 41.794° | 2026-06-16 05:19:08.232Z | 58.093° ENE |
| 6 mins | 2026-06-16 06:54:08.232Z | 286.665° WNW | 2026-06-16 06:57:08.232Z | 348.158° N | 26.62° | 2026-06-16 07:00:08.232Z | 35.023° NE |
| 4 mins | 2026-06-16 08:38:08.232Z | 338.76° N | 2026-06-16 08:39:08.232Z | 355.133° N | 17.199° | 2026-06-16 08:42:08.232Z | 38.629° NE |
| 5 mins | 2026-06-16 10:20:08.232Z | 343.157° N | 2026-06-16 10:22:08.232Z | 22.565° NE | 23.658° | 2026-06-16 10:25:08.232Z | 71.166° E |
| 7 mins | 2026-06-16 12:01:08.232Z | 307.172° NW | 2026-06-16 12:04:08.232Z | 142.302° SSE | 44.724° | 2026-06-16 12:08:08.232Z | 129.889° SE |
| 5 mins | 2026-06-17 03:52:08.232Z | 163.859° S | 2026-06-17 03:54:08.232Z | 129.9° SE | 20.309° | 2026-06-17 03:57:08.232Z | 83.905° 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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