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, 14.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR-2 IRINA
1 68480U 26067BS 26217.39028865 .00001925 00000-0 18963-3 0 9993
2 68480 97.7657 175.1498 0005536 99.9983 260.1861 14.93214589 19077Epoch: 2026-08-05T09:22Z
TLE epoch observation values (Epoch: 2026-08-05T09:22:00.939Z)
Latitude
-0.00006°
Longitude
80.70052°
Altitude
591.623 km
Speed
7.564 km/s
True Right ascension
11h 40m 35s
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
16:18:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.792 km
Perigee altitude
581.082 km
Semi-major axis
6,963.074 km
Eccentricity
0.00055
Inclination
97.7657°
RAAN
175.1498°
Arg. of periapsis
99.9983°
True anomaly
260.1236°
Mean anomaly
260.1861°
Eccentric anomaly
260.15485°
Mean motion
3.73544 °/min
Orbital period
96.37 mins
BSTAR
0.00018963
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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 | 2026-08-06 10:03:18.163Z | 15.27° NNE | 2026-08-06 10:07:18.163Z | 164.336° S | 43.035° | 2026-08-06 10:10:18.163Z | 189.029° SSW |
| 6 mins | 2026-08-06 20:53:18.163Z | 140.114° SSE | 2026-08-06 20:56:18.163Z | 58.98° ENE | 35.757° | 2026-08-06 20:59:18.163Z | 2.788° 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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