LEMUR-2 IRINA, 68480
Orbit data source: Space-Track
LEMUR-2 IRINA, 68480 is a payload satellite owned by Spire (LU) in SSO that was launched on Mon, 30 Mar 2026 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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Identifier
Orbit
Country
LU / LUXERelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LEMUR-2 IRINA
1 68480U 26067BS 26263.42388686 .00002150 00000-0 21014-3 0 9990
2 68480 97.7728 220.6351 0003043 340.9767 19.1339 14.93412973 25942Epoch: 2026-09-20T10:10Z
TLE epoch observation values (Epoch: 2026-09-20T10:10:23.824Z)
Latitude
0.00002°
Longitude
68.71756°
Altitude
588.344 km
Speed
7.567 km/s
True Right ascension
14h 42m 32s
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
12:54:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.439 km
Perigee altitude
582.202 km
Semi-major axis
6,962.457 km
Eccentricity
0.0003
Inclination
97.7728°
RAAN
220.6351°
Arg. of periapsis
340.9767°
True anomaly
19.14533°
Mean anomaly
19.1339°
Eccentric anomaly
19.13962°
Mean motion
3.73594 °/min
Orbital period
96.36 mins
BSTAR
0.00021014
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Other satellites on launch #67 in the year 2026 (2026-03-30 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 IRINA 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 | 2026-09-20 21:33:30.700Z | 185.497° SSW | 2026-09-20 21:36:30.700Z | 269.881° W | 55.996° | 2026-09-20 21:39:30.700Z | 335.394° NNW |
| 4 mins | 2026-09-21 09:17:30.700Z | 65.477° ENE | 2026-09-21 09:18:30.700Z | 84.418° E | 21.294° | 2026-09-21 09:21:30.700Z | 138.513° SSE |
| 5 mins | 2026-09-21 10:52:30.700Z | 332.344° NNW | 2026-09-21 10:54:30.700Z | 287.845° WNW | 28.687° | 2026-09-21 10:57:30.700Z | 234.241° WSW |
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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