KUIPER-00203, 67773
Orbit data source: Space-Track
KUIPER-00203, 67773 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 12 Feb 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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67773 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00203
1 67773U 26030K 26170.85287280 .00002429 00000-0 34743-3 0 9998
2 67773 51.9055 126.3874 0000822 72.0616 288.0436 14.79935923 20232Epoch: 2026-06-19T20:28Z
TLE epoch observation values (Epoch: 2026-06-19T20:28:08.209Z)
Latitude
-0.00004°
Longitude
-88.72273°
Altitude
630.095 km
Speed
7.545 km/s
True Right ascension
08h 25m 32s
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
10:19:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.553 km
Perigee altitude
629.401 km
Semi-major axis
7,008.114 km
Eccentricity
0.00008
Inclination
51.9055°
RAAN
126.3874°
Arg. of periapsis
72.0616°
True anomaly
288.03464°
Mean anomaly
288.0436°
Eccentric anomaly
288.03912°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00034743
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Other satellites on launch #30 in the year 2026 (2026-02-12 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-00203 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 00:13:28.854Z | 247.335° WSW | 2026-06-21 00:17:28.854Z | 357.913° N | 40.221° | 2026-06-21 00:21:28.854Z | 47.256° ENE |
| 5 mins | 2026-06-21 01:57:28.854Z | 315.465° NNW | 2026-06-21 01:59:28.854Z | 351.422° N | 20.248° | 2026-06-21 02:02:28.854Z | 34.687° NE |
| 4 mins | 2026-06-21 03:40:28.854Z | 343.03° N | 2026-06-21 03:41:28.854Z | 359.217° N | 17.784° | 2026-06-21 03:44:28.854Z | 45.881° ENE |
| 7 mins | 2026-06-21 05:21:28.854Z | 326.441° NNW | 2026-06-21 05:24:28.854Z | 31.151° NE | 33.02° | 2026-06-21 05:28:28.854Z | 98.093° ESE |
| 6 mins | 2026-06-21 07:03:28.854Z | 281.592° WNW | 2026-06-21 07:05:28.854Z | 239.552° WSW | 32.198° | 2026-06-21 07:09:28.854Z | 160.242° S |
| 6 mins | 2026-06-21 22:53:28.854Z | 199.52° SSW | 2026-06-21 22:55:28.854Z | 157.341° SSE | 36.033° | 2026-06-21 22:59:28.854Z | 65.237° ENE |
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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