IRIDE-MS1-EAG2-12, 68461
Orbit data source: Space-Track
IRIDE-MS1-EAG2-12, 68461 is an Italian payload satellite 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
ITRelated business
Manufacturer
OHB-I
Mission
Operational Commercial Technology
Bus & Motor
EAGLET, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.368 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 IRIDE-MS1-EAG2-12
1 68461U 26067AX 26263.43894281 .00005232 00000-0 25211-3 0 9990
2 68461 97.4648 220.6023 0006117 90.3847 269.8088 15.19144497 26392Epoch: 2026-09-20T10:32Z
TLE epoch observation values (Epoch: 2026-09-20T10:32:04.658Z)
Latitude
-0.00009°
Longitude
63.24979°
Altitude
511.529 km
Speed
7.608 km/s
True Right ascension
14h 42m 24s
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
18:55:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.605 km
Perigee altitude
501.184 km
Semi-major axis
6,883.531 km
Eccentricity
0.00061
Inclination
97.4648°
RAAN
220.6023°
Arg. of periapsis
90.3847°
True anomaly
269.7387°
Mean anomaly
269.8088°
Eccentric anomaly
269.77375°
Mean motion
3.80037 °/min
Orbital period
94.73 mins
BSTAR
0.00025211
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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.IRIDE-MS1-EAG2-12 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-21 09:15:06.357Z | 56.419° ENE | 2026-09-21 09:17:06.357Z | 93.511° ESE | 18.211° | 2026-09-21 09:19:06.357Z | 131.053° SE |
| 5 mins | 2026-09-21 10:49:06.357Z | 333.501° NNW | 2026-09-21 10:51:06.357Z | 286.989° WNW | 26.451° | 2026-09-21 10:54:06.357Z | 231.701° WSW |
| 5 mins | 2026-09-21 21:27:06.357Z | 179.791° S | 2026-09-21 21:29:06.357Z | 239.842° WSW | 67.481° | 2026-09-21 21:32:06.357Z | 340.79° N |
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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