Showing default

FLYLAB 1, 68472

Orbit data source: Space-Track

FLYLAB 1, 68472 is a payload satellite owned by ONERA (FR) 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
68472, 2026-067BJ
Orbit
SSO
Country
Flag of FRFR
Related business
Manufacturer
NanoAvionics
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
15 kg wet, ~15 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 + 4 Pan, 1.0 m
Radar Cross Section
0.159 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FLYLAB 1
1 68472U 26067BJ  26216.41467343  .00002096  00000-0  21690-3 0  9995
2 68472  97.7651 173.8127 0001840 250.0089 110.0931 14.91128687 18911
Epoch: 2026-08-04T09:57Z
TLE epoch observation values (Epoch: 2026-08-04T09:57:07.784Z)
Latitude
-0.00005°
Longitude
71.54651°
Altitude
597.897 km
Speed
7.561 km/s
True Right ascension
11h 35m 15s
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
14:22:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.717 km
Perigee altitude
590.153 km
Semi-major axis
6,969.572 km
Eccentricity
0.00018
Inclination
97.7651°
RAAN
173.8127°
Arg. of periapsis
250.0089°
True anomaly
110.1129°
Mean anomaly
110.0931°
Eccentric anomaly
110.103°
Mean motion
3.73022 °/min
Orbital period
96.51 mins
BSTAR
0.0002169
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
|