SPOQC, 68423
Orbit data source: Space-Track
SPOQC, 68423 is a Dutch payload satellite in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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68423 intel report (Beta)
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Identifier
Orbit
Country
NL / NETHRelated business
Manufacturer
ISIS BV
Mission
Operational Amateur Communications
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 SPOQC
1 68423U 26067H 26308.19458400 .00003132 00000-0 14878-3 0 9994
2 68423 97.4703 264.9686 0002371 101.6917 258.4584 15.19958171 33205Epoch: 2026-11-04T04:40Z
TLE epoch observation values (Epoch: 2026-11-04T04:40:12.057Z)
Latitude
-0.00004°
Longitude
151.47197°
Altitude
509.382 km
Speed
7.609 km/s
True Right ascension
17h 39m 52s
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
15:33:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.567 km
Perigee altitude
501.304 km
Semi-major axis
6,881.073 km
Eccentricity
0.00024
Inclination
97.4703°
RAAN
264.9686°
Arg. of periapsis
101.6917°
True anomaly
258.43178°
Mean anomaly
258.4584°
Eccentric anomaly
258.44509°
Mean motion
3.80241 °/min
Orbital period
94.68 mins
BSTAR
0.00014878
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.SPOQC 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-04 20:36:41.681Z | 122.948° SE | 2026-11-04 20:39:41.681Z | 61° ENE | 24.873° | 2026-11-04 20:41:41.681Z | 21.748° NNE |
| 4 mins | 2026-11-04 22:11:41.681Z | 235.422° WSW | 2026-11-04 22:12:41.681Z | 254.976° W | 18.638° | 2026-11-04 22:15:41.681Z | 310.586° NW |
| 5 mins | 2026-11-05 09:41:41.681Z | 43.765° NE | 2026-11-05 09:43:41.681Z | 101.631° ESE | 36.791° | 2026-11-05 09:46:41.681Z | 164.584° S |
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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