LEMUR 2 KADI, 43184
Orbit data source: Space-Track
LEMUR 2 KADI, 43184 is a payload satellite owned by Spire (US) in SSO that was launched on Thu, 01 Feb 2018 UTC via a SOYUZ-2-1A launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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43184 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.124 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 LEMUR 2 KADI
1 43184U 18014E 25309.53784313 .00056230 00000-0 11506-2 0 9998
2 43184 97.4941 223.6584 0006313 29.1086 331.0513 15.45913102426105Epoch: 2025-11-05T12:54Z
TLE epoch observation values (Epoch: 2025-11-05T12:54:29.646Z)
Latitude
-0.00009°
Longitude
-14.9742°
Altitude
428.059 km
Speed
7.657 km/s
True Right ascension
14h 54m 38s
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
05:55:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.927 km
Perigee altitude
421.336 km
Semi-major axis
6,803.769 km
Eccentricity
0.00063
Inclination
97.4941°
RAAN
223.6584°
Arg. of periapsis
29.1086°
True anomaly
331.01626°
Mean anomaly
331.0513°
Eccentric anomaly
331.03378°
Mean motion
3.8674 °/min
Orbital period
93.09 mins
BSTAR
0.0011506
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Other satellites on launch #14 in the year 2018 (2018-02-01 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.LEMUR 2 KADI 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 | 2025-11-06 18:32:42.764Z | 172.997° S | 2025-11-06 18:35:42.764Z | 253.993° W | 43.766° | 2025-11-06 18:38:42.764Z | 343.667° N |
| 4 mins | 2025-11-07 07:25:42.764Z | 0.082° NNE | 2025-11-07 07:26:42.764Z | 328.5° NNW | 42.098° | 2025-11-07 07:29:42.764Z | 200.482° SSW |
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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