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.
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43804 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
Aalto univ.
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 SUOMI100
1 43804U 18099AY 26235.41102571 .00010094 00000-0 35130-3 0 9994
2 43804 97.4135 295.6008 0010650 50.6036 309.6145 15.29837450423698Epoch: 2026-08-23T09:51Z
TLE epoch observation values (Epoch: 2026-08-23T09:51:52.621Z)
Latitude
-0.0001°
Longitude
175.92409°
Altitude
474.75 km
Speed
7.631 km/s
True Right ascension
19h 42m 24s
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
21:34:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.548 km
Perigee altitude
465.954 km
Semi-major axis
6,851.388 km
Eccentricity
0.00107
Inclination
97.4135°
RAAN
295.6008°
Arg. of periapsis
50.6036°
True anomaly
309.52041°
Mean anomaly
309.6145°
Eccentric anomaly
309.56746°
Mean motion
3.82715 °/min
Orbital period
94.06 mins
BSTAR
0.0003513
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.SUOMI100 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 | 2026-08-24 16:15:51.293Z | 46.787° ENE | 2026-08-24 16:17:51.293Z | 85.449° E | 20.794° | 2026-08-24 16:20:51.293Z | 147.418° SSE |
| 4 mins | 2026-08-24 17:49:51.293Z | 322.649° NNW | 2026-08-24 17:51:51.293Z | 279.181° WNW | 17.653° | 2026-08-24 17:53:51.293Z | 244.752° WSW |
| 4 mins | 2026-08-25 04:23:51.293Z | 195.27° SSW | 2026-08-25 04:24:51.293Z | 227.716° WSW | 37.72° | 2026-08-25 04:27:51.293Z | 335.223° NNW |
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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