KUIPER-00077, 64824
Orbit data source: Space-Track
KUIPER-00077, 64824 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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64824 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: 7 hours ago
TLE from 7 hours ago
0 KUIPER-00077
1 64824U 25151J 26166.88355302 .00002237 00000-0 32257-3 0 9999
2 64824 51.9007 223.8993 0000620 89.8938 270.2095 14.79910535 49885Epoch: 2026-06-15T21:12Z
TLE epoch observation values (Epoch: 2026-06-15T21:12:18.980Z)
Latitude
-0.00007°
Longitude
1.65661°
Altitude
630.352 km
Speed
7.544 km/s
True Right ascension
14h 55m 35s
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
14:43:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.492 km
Perigee altitude
629.623 km
Semi-major axis
7,008.195 km
Eccentricity
0.00006
Inclination
51.9007°
RAAN
223.8993°
Arg. of periapsis
89.8938°
True anomaly
270.2024°
Mean anomaly
270.2095°
Eccentric anomaly
270.20595°
Mean motion
3.69942 °/min
Orbital period
97.31 mins
BSTAR
0.00032257
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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-00077 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 05:27:11.917Z | 171.855° S | 2026-06-16 05:30:11.917Z | 127.196° SE | 18.975° | 2026-06-16 05:33:11.917Z | 83.816° E |
| 7 mins | 2026-06-16 07:08:11.917Z | 244.104° WSW | 2026-06-16 07:11:11.917Z | 323.622° NNW | 43.129° | 2026-06-16 07:15:11.917Z | 47.749° ENE |
| 5 mins | 2026-06-16 08:51:11.917Z | 307.105° NW | 2026-06-16 08:53:11.917Z | 341.663° N | 21.166° | 2026-06-16 08:56:11.917Z | 30.076° NE |
| 5 mins | 2026-06-16 10:34:11.917Z | 336.024° NNW | 2026-06-16 10:36:11.917Z | 7.999° NNE | 17.696° | 2026-06-16 10:39:11.917Z | 50.105° ENE |
| 6 mins | 2026-06-16 12:16:11.917Z | 333.244° NNW | 2026-06-16 12:18:11.917Z | 14.744° NNE | 30.734° | 2026-06-16 12:22:11.917Z | 91.744° ESE |
| 7 mins | 2026-06-16 13:57:11.917Z | 289.824° WNW | 2026-06-16 14:00:11.917Z | 222.143° SW | 35.601° | 2026-06-16 14:04:11.917Z | 153.285° SSE |
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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