IRIDE-MS1-EAG2-10, 68451
Orbit data source: Space-Track
IRIDE-MS1-EAG2-10, 68451 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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68451 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
OHB-I
Mission
Operational spacecraft
Bus & Motor
EAGLET, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.0 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 IRIDE-MS1-EAG2-10
1 68451U 26067AM 26171.35216389 .00006566 00000-0 31741-3 0 9991
2 68451 97.4503 129.7731 0002709 63.9393 296.2120 15.18949338 12427Epoch: 2026-06-20T08:27Z
TLE epoch observation values (Epoch: 2026-06-20T08:27:06.960Z)
Latitude
-0°
Longitude
94.42608°
Altitude
511.278 km
Speed
7.609 km/s
True Right ascension
08h 39m 05s
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
15:13:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.849 km
Perigee altitude
504.119 km
Semi-major axis
6,884.121 km
Eccentricity
0.00027
Inclination
97.4503°
RAAN
129.7731°
Arg. of periapsis
63.9393°
True anomaly
296.18415°
Mean anomaly
296.212°
Eccentric anomaly
296.19807°
Mean motion
3.79988 °/min
Orbital period
94.74 mins
BSTAR
0.00031741
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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-EAG2-10 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 10:01:41.016Z | 16.491° NNE | 2026-06-22 10:04:41.016Z | 107.289° ESE | 44.087° | 2026-06-22 10:07:41.016Z | 186.846° SSW |
| 4 mins | 2026-06-22 20:41:41.016Z | 106.5° ESE | 2026-06-22 20:42:41.016Z | 80.018° E | 25.388° | 2026-06-22 20:45:41.016Z | 15.126° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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