Showing default

SUOMI100, 43804

Orbit data source: Space-Track

SUOMI100, 43804 is a payload satellite owned by Aalto univ. (FI) in SSO that was launched on Mon, 03 Dec 2018 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
43804, 2018-099AY
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
Aalto univ.
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2018-12-03 (7 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)

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

TLE from 1 day ago
0 SUOMI100
1 43804U 18099AY  26034.11397577  .00014618  00000-0  58762-3 0  9992
2 43804  97.4395  95.2005 0011349  39.7444 320.4623 15.24968247392965
Epoch: 2026-02-03T02:44Z
TLE epoch observation values (Epoch: 2026-02-03T02:44:07.506Z)
Latitude
-0.00004°
Longitude
-79.13033°
Altitude
487.967 km
Speed
7.624 km/s
True Right ascension
06h 20m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:44:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.634 km
Perigee altitude
480.049 km
Semi-major axis
6,865.978 km
Eccentricity
0.00113
Inclination
97.4395°
RAAN
95.2005°
Arg. of periapsis
39.7444°
True anomaly
320.37942°
Mean anomaly
320.4623°
Eccentric anomaly
320.42087°
Mean motion
3.81496 °/min
Orbital period
94.37 mins
BSTAR
0.00058762
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|