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: 9 hours ago
TLE from 9 hours ago
0 LEMUR-2 IRINA
1 68480U 26067BS 26260.14076682 .00002395 00000-0 23351-3 0 9993
2 68480 97.7724 217.3890 0003436 350.7723 9.3433 14.93401574 25453Epoch: 2026-09-17T03:22Z
TLE epoch observation values (Epoch: 2026-09-17T03:22:42.253Z)
Latitude
0°
Longitude
170.63067°
Altitude
588.02 km
Speed
7.567 km/s
True Right ascension
14h 29m 33s
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
05:13:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.748 km
Perigee altitude
581.964 km
Semi-major axis
6,962.493 km
Eccentricity
0.00034
Inclination
97.7724°
RAAN
217.389°
Arg. of periapsis
350.7723°
True anomaly
9.3497°
Mean anomaly
9.3433°
Eccentric anomaly
9.3465°
Mean motion
3.73591 °/min
Orbital period
96.36 mins
BSTAR
0.00023351
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-17 21:10:50.945Z | 162.295° S | 2026-09-17 21:14:50.945Z | 73.228° E | 79.434° | 2026-09-17 21:18:50.945Z | 350.283° N |
| 6 mins | 2026-09-18 10:30:50.945Z | 350.332° N | 2026-09-18 10:32:50.945Z | 295.992° NW | 49.57° | 2026-09-18 10:36:50.945Z | 212.108° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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