KUIPER-00420, 68932
Orbit data source: Space-Track
KUIPER-00420, 68932 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 30 Apr 2026 UTC via an ARIANE 64 launch vehicle from the French Guiana (FRGUI). 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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68932 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 KUIPER-00420
1 68932U 26098P 26155.13063746 .00040951 00000-0 11684-2 0 9993
2 68932 51.8769 130.5056 0003709 107.8246 252.3145 15.35635641 5346Epoch: 2026-06-04T03:08Z
TLE epoch observation values (Epoch: 2026-06-04T03:08:07.076Z)
Latitude
-0.00001°
Longitude
-169.10321°
Altitude
460.567 km
Speed
7.637 km/s
True Right ascension
08h 42m 01s
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
03:05:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.035 km
Perigee altitude
456.963 km
Semi-major axis
6,837.636 km
Eccentricity
0.00037
Inclination
51.8769°
RAAN
130.5056°
Arg. of periapsis
107.8246°
True anomaly
252.27401°
Mean anomaly
252.3145°
Eccentric anomaly
252.29426°
Mean motion
3.8387 °/min
Orbital period
93.78 mins
BSTAR
0.0011684
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Other satellites on launch #98 in the year 2026 (2026-04-30 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-00420 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 | 2026-06-07 00:01:17.884Z | 212.997° SW | 2026-06-07 00:04:17.884Z | 144.001° SSE | 38.125° | 2026-06-07 00:07:17.884Z | 63.3° ENE |
| 4 mins | 2026-06-07 01:40:17.884Z | 290.344° WNW | 2026-06-07 01:42:17.884Z | 337.812° N | 23.009° | 2026-06-07 01:44:17.884Z | 22.582° NE |
| 5 mins | 2026-06-07 06:36:17.884Z | 323.772° NNW | 2026-06-07 06:38:17.884Z | 76.552° E | 39.531° | 2026-06-07 06:41:17.884Z | 117.352° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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