Showing default

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.

Loading next visibility...
Identifier
68423, 2026-067H
Orbit
SSO
Country
Flag of NLNL / NETH
Related business
Manufacturer
ISIS BV
Mission
Operational Amateur Communications
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2026-03-30 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SPOQC
1 68423U 26067H   26259.33992098  .00004432  00000-0  21157-3 0  9993
2 68423  97.4612 216.6381 0001571  70.9390 289.2014 15.19570387 25787
Epoch: 2026-09-16T08:09Z
TLE epoch observation values (Epoch: 2026-09-16T08:09:29.172Z)
Latitude
-0.00012°
Longitude
98.97364°
Altitude
509.871 km
Speed
7.609 km/s
True Right ascension
14h 26m 33s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
03:00:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.188 km
Perigee altitude
503.026 km
Semi-major axis
6,882.244 km
Eccentricity
0.00016
Inclination
97.4612°
RAAN
216.6381°
Arg. of periapsis
70.939°
True anomaly
289.1844°
Mean anomaly
289.2014°
Eccentric anomaly
289.1929°
Mean motion
3.80144 °/min
Orbital period
94.7 mins
BSTAR
0.00021157
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|