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: 5 days ago
TLE from 5 days ago
0 SUOMI100
1 43804U 18099AY 26155.11113851 .00014467 00000-0 52952-3 0 9994
2 43804 97.4190 215.5556 0008831 333.9373 26.1421 15.28111453411420Epoch: 2026-06-04T02:40Z
TLE epoch observation values (Epoch: 2026-06-04T02:40:02.367Z)
Latitude
0.00002°
Longitude
-77.01436°
Altitude
479.121 km
Speed
7.629 km/s
True Right ascension
14h 22m 13s
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
19:05:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.469 km
Perigee altitude
472.359 km
Semi-major axis
6,856.551 km
Eccentricity
0.00088
Inclination
97.419°
RAAN
215.5556°
Arg. of periapsis
333.9373°
True anomaly
26.18673°
Mean anomaly
26.1421°
Eccentric anomaly
26.16441°
Mean motion
3.82283 °/min
Orbital period
94.17 mins
BSTAR
0.00052952
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-09 16:48:02.534Z | 16.354° NNE | 2026-06-09 16:51:02.534Z | 63.296° ENE | 43.093° | 2026-06-09 16:54:02.534Z | 185.498° SSW |
| 4 mins | 2026-06-10 03:24:02.534Z | 110.584° ESE | 2026-06-10 03:26:02.534Z | 62.152° ENE | 21.923° | 2026-06-10 03:28:02.534Z | 22.07° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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