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 spacecraft
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
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR-2 IRINA
1 68480U 26067BS 26171.34962918 .00002717 00000-0 26719-3 0 9991
2 68480 97.7623 129.7029 0002036 255.7809 104.3184 14.92947331 12208Epoch: 2026-06-20T08:23Z
TLE epoch observation values (Epoch: 2026-06-20T08:23:27.961Z)
Latitude
-0.00003°
Longitude
95.27088°
Altitude
592.146 km
Speed
7.564 km/s
True Right ascension
08h 38m 48s
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
07:29:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.187 km
Perigee altitude
584.351 km
Semi-major axis
6,963.906 km
Eccentricity
0.0002
Inclination
97.7623°
RAAN
129.7029°
Arg. of periapsis
255.7809°
True anomaly
104.341°
Mean anomaly
104.3184°
Eccentric anomaly
104.3297°
Mean motion
3.73477 °/min
Orbital period
96.39 mins
BSTAR
0.00026719
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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 | 2026-06-21 21:29:59.551Z | 179.53° S | 2026-06-21 21:33:59.551Z | 266.747° W | 40.626° | 2026-06-21 21:36:59.551Z | 336.348° NNW |
| 4 mins | 2026-06-22 09:14:59.551Z | 62.467° ENE | 2026-06-22 09:16:59.551Z | 100.675° ESE | 19.356° | 2026-06-22 09:18:59.551Z | 134.783° SE |
| 5 mins | 2026-06-22 10:49:59.551Z | 336.913° NNW | 2026-06-22 10:51:59.551Z | 295.1° NW | 26.218° | 2026-06-22 10:54:59.551Z | 235.436° 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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