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: 22 hours ago
TLE from 22 hours ago
0 SUOMI100
1 43804U 18099AY 26184.70259162 .00014005 00000-0 50200-3 0 9999
2 43804 97.4171 245.0375 0009372 212.7004 147.3657 15.28800766415942Epoch: 2026-07-03T16:51Z
TLE epoch observation values (Epoch: 2026-07-03T16:51:43.915Z)
Latitude
-0.00003°
Longitude
70.37769°
Altitude
487.913 km
Speed
7.618 km/s
True Right ascension
16h 20m 09s
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
03:09:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.775 km
Perigee altitude
469.927 km
Semi-major axis
6,854.488 km
Eccentricity
0.00094
Inclination
97.4171°
RAAN
245.0375°
Arg. of periapsis
212.7004°
True anomaly
147.42356°
Mean anomaly
147.3657°
Eccentric anomaly
147.39463°
Mean motion
3.82455 °/min
Orbital period
94.13 mins
BSTAR
0.000502
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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 | 2026-07-04 16:59:12.461Z | 9.275° NNE | 2026-07-04 17:02:12.461Z | 237.668° WSW | 44.292° | 2026-07-04 17:05:12.461Z | 196.393° SSW |
| 5 mins | 2026-07-05 03:34:12.461Z | 124.068° SE | 2026-07-05 03:36:12.461Z | 72.85° E | 27.572° | 2026-07-05 03:39:12.461Z | 10.323° 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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