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 (4 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: 14 hours ago

TLE from 14 hours ago
0 SPOQC
1 68423U 26067H   26217.45486312  .00003228  00000-0  15630-3 0  9998
2 68423  97.4540 175.2686 0002703  94.4086 265.7458 15.19269027 19427
Epoch: 2026-08-05T10:55Z
TLE epoch observation values (Epoch: 2026-08-05T10:55:00.173Z)
Latitude
0.00003°
Longitude
57.50885°
Altitude
511.275 km
Speed
7.608 km/s
True Right ascension
11h 41m 04s
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
14:25:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.878 km
Perigee altitude
503.157 km
Semi-major axis
6,883.154 km
Eccentricity
0.00027
Inclination
97.454°
RAAN
175.2686°
Arg. of periapsis
94.4086°
True anomaly
265.71491°
Mean anomaly
265.7458°
Eccentric anomaly
265.73036°
Mean motion
3.80069 °/min
Orbital period
94.72 mins
BSTAR
0.0001563
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
|