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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SUOMI100
1 43804U 18099AY 25286.24441509 .00020063 00000-0 89963-3 0 9997
2 43804 97.4575 343.2424 0012909 73.2627 287.0024 15.21175634375786Epoch: 2025-10-13T05:51Z
TLE epoch observation values (Epoch: 2025-10-13T05:51:57.463Z)
Latitude
-0.00006°
Longitude
-126.797°
Altitude
502.797 km
Speed
7.614 km/s
True Right ascension
22h 52m 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
11:53:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.138 km
Perigee altitude
490.382 km
Semi-major axis
6,877.397 km
Eccentricity
0.00129
Inclination
97.4575°
RAAN
343.2424°
Arg. of periapsis
73.2627°
True anomaly
286.86087°
Mean anomaly
287.0024°
Eccentric anomaly
286.93164°
Mean motion
3.80546 °/min
Orbital period
94.6 mins
BSTAR
0.00089963
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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 | 2025-10-13 17:29:00.980Z | 335.743° NNW | 2025-10-13 17:31:00.980Z | 291.778° WNW | 23.423° | 2025-10-13 17:34:00.980Z | 233.329° WSW |
| 6 mins | 2025-10-14 04:06:00.980Z | 177.567° S | 2025-10-14 04:09:00.980Z | 307.164° NW | 40.797° | 2025-10-14 04:12:00.980Z | 342.69° N |
| 6 mins | 2025-10-14 17:09:00.980Z | 357.352° N | 2025-10-14 17:12:00.980Z | 296.834° NW | 34.697° | 2025-10-14 17:15:00.980Z | 217.136° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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