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, 0.087 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SUOMI100
1 43804U 18099AY 26295.69396894 .00014080 00000-0 47022-3 0 9995
2 43804 97.4041 355.7436 0009455 178.0182 182.1098 15.31101392432913Epoch: 2026-10-22T16:39Z
TLE epoch observation values (Epoch: 2026-10-22T16:39:18.916Z)
Latitude
-0.00005°
Longitude
74.7896°
Altitude
482.105 km
Speed
7.621 km/s
True Right ascension
23h 42m 58s
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
13:18:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.95 km
Perigee altitude
463.002 km
Semi-major axis
6,847.613 km
Eccentricity
0.00095
Inclination
97.4041°
RAAN
355.7436°
Arg. of periapsis
178.0182°
True anomaly
182.10582°
Mean anomaly
182.1098°
Eccentric anomaly
182.10781°
Mean motion
3.83031 °/min
Orbital period
93.99 mins
BSTAR
0.00047022
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-24 03:18:56.953Z | 107.62° ESE | 2026-10-24 03:20:56.953Z | 69.956° E | 17.86° | 2026-10-24 03:22:56.953Z | 31.479° NE |
| 4 mins | 2026-10-24 04:52:56.953Z | 235.38° WSW | 2026-10-24 04:53:56.953Z | 262.066° W | 24.936° | 2026-10-24 04:56:56.953Z | 320.738° NNW |
| 4 mins | 2026-10-24 16:17:56.953Z | 60.809° ENE | 2026-10-24 16:18:56.953Z | 82.533° E | 20.817° | 2026-10-24 16:21:56.953Z | 144.788° SSE |
| 4 mins | 2026-10-24 17:50:56.953Z | 324.301° NNW | 2026-10-24 17:52:56.953Z | 279.994° WNW | 19.272° | 2026-10-24 17:54:56.953Z | 244.216° WSW |
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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