IRIDE-MS1-EAG2-13, 68450
Orbit data source: Space-Track
IRIDE-MS1-EAG2-13, 68450 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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68450 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: 15 hours ago
TLE from 15 hours ago
0 IRIDE-MS1-EAG2-13
1 68450U 26067AL 26217.46441382 .00004800 00000-0 23020-3 0 9996
2 68450 97.4576 175.3281 0002178 155.3736 204.7603 15.19368591 19424Epoch: 2026-08-05T11:08Z
TLE epoch observation values (Epoch: 2026-08-05T11:08:45.354Z)
Latitude
0°
Longitude
54.12069°
Altitude
512.198 km
Speed
7.607 km/s
True Right ascension
11h 41m 18s
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
16:18:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.216 km
Perigee altitude
503.217 km
Semi-major axis
6,882.854 km
Eccentricity
0.00022
Inclination
97.4576°
RAAN
175.3281°
Arg. of periapsis
155.3736°
True anomaly
204.74985°
Mean anomaly
204.7603°
Eccentric anomaly
204.75507°
Mean motion
3.80093 °/min
Orbital period
94.71 mins
BSTAR
0.0002302
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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-EAG2-13 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 | 2026-08-06 09:50:38.400Z | 26.556° NE | 2026-08-06 09:53:38.400Z | 115.523° SE | 37.532° | 2026-08-06 09:56:38.400Z | 175.597° S |
| 4 mins | 2026-08-06 20:29:38.400Z | 109.289° ESE | 2026-08-06 20:31:38.400Z | 68.888° E | 19.801° | 2026-08-06 20:33:38.400Z | 28.98° NE |
| 4 mins | 2026-08-06 22:03:38.400Z | 225.98° WSW | 2026-08-06 22:05:38.400Z | 270.899° WNW | 21.165° | 2026-08-06 22:07:38.400Z | 310.27° NW |
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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