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 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: 21 hours ago
TLE from 21 hours ago
0 IRIDE-MS1-EAG2-10
1 68451U 26067AM 26217.39274252 .00004839 00000-0 23147-3 0 9991
2 68451 97.4537 175.1996 0001859 137.1021 223.0358 15.19449667 19417Epoch: 2026-08-05T09:25Z
TLE epoch observation values (Epoch: 2026-08-05T09:25:32.953Z)
Latitude
-0.00014°
Longitude
79.86452°
Altitude
511.527 km
Speed
7.608 km/s
True Right ascension
11h 40m 47s
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
20:27:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.751 km
Perigee altitude
503.192 km
Semi-major axis
6,882.608 km
Eccentricity
0.00019
Inclination
97.4537°
RAAN
175.1996°
Arg. of periapsis
137.1021°
True anomaly
223.02126°
Mean anomaly
223.0358°
Eccentric anomaly
223.02853°
Mean motion
3.80114 °/min
Orbital period
94.71 mins
BSTAR
0.00023147
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-06 09:42:31.786Z | 35.002° NE | 2026-08-06 09:44:31.786Z | 77.643° E | 31.344° | 2026-08-06 09:47:31.786Z | 162.36° S |
| 4 mins | 2026-08-06 21:55:31.786Z | 224.994° SW | 2026-08-06 21:56:31.786Z | 250.231° W | 25.149° | 2026-08-06 21:59:31.786Z | 318.71° NNW |
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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