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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68480 intel report (Beta)
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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: 21 hours ago
TLE from 21 hours ago
0 LEMUR-2 IRINA
1 68480U 26067BS 26255.38354809 .00002111 00000-0 20651-3 0 9999
2 68480 97.7719 212.6865 0003953 8.7453 351.3834 14.93383229 24743Epoch: 2026-09-12T09:12Z
TLE epoch observation values (Epoch: 2026-09-12T09:12:18.554Z)
Latitude
-0.00013°
Longitude
83.21588°
Altitude
587.716 km
Speed
7.568 km/s
True Right ascension
14h 10m 44s
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
22:21:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.165 km
Perigee altitude
581.661 km
Semi-major axis
6,962.55 km
Eccentricity
0.0004
Inclination
97.7719°
RAAN
212.6865°
Arg. of periapsis
8.7453°
True anomaly
351.37661°
Mean anomaly
351.3834°
Eccentric anomaly
351.38001°
Mean motion
3.73586 °/min
Orbital period
96.36 mins
BSTAR
0.00020651
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-13 09:53:56.920Z | 22.969° NE | 2026-09-13 09:56:56.920Z | 85.936° E | 59.267° | 2026-09-13 10:00:56.920Z | 180.528° SSW |
| 6 mins | 2026-09-13 20:43:56.920Z | 125.168° SE | 2026-09-13 20:45:56.920Z | 79.953° E | 35.568° | 2026-09-13 20:49:56.920Z | 5.53° NNE |
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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