IRIDE-MS1-EAG2-11, 68453
Orbit data source: Space-Track
IRIDE-MS1-EAG2-11, 68453 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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68453 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: 1 day ago
TLE from 1 day ago
0 IRIDE-MS1-EAG2-11
1 68453U 26067AP 26234.85080295 .00006457 00000-0 30649-3 0 9998
2 68453 97.4597 192.5103 0003789 119.9048 240.2563 15.19591626 22066Epoch: 2026-08-22T20:25Z
TLE epoch observation values (Epoch: 2026-08-22T20:25:09.374Z)
Latitude
-0.0001°
Longitude
-84.93403°
Altitude
511.457 km
Speed
7.607 km/s
True Right ascension
12h 50m 02s
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
14:02:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.65 km
Perigee altitude
501.435 km
Semi-major axis
6,882.18 km
Eccentricity
0.00038
Inclination
97.4597°
RAAN
192.5103°
Arg. of periapsis
119.9048°
True anomaly
240.21861°
Mean anomaly
240.2563°
Eccentric anomaly
240.23745°
Mean motion
3.80149 °/min
Orbital period
94.7 mins
BSTAR
0.00030649
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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-EAG2-11 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 | 2026-08-24 09:20:40.153Z | 47.892° ENE | 2026-08-24 09:23:40.153Z | 106.734° ESE | 19.24° | 2026-08-24 09:25:40.153Z | 141.936° SSE |
| 4 mins | 2026-08-24 10:55:40.153Z | 320.495° NNW | 2026-08-24 10:56:40.153Z | 297.95° NW | 20.864° | 2026-08-24 10:59:40.153Z | 239.59° WSW |
| 6 mins | 2026-08-24 21:32:40.153Z | 185.518° SSW | 2026-08-24 21:34:40.153Z | 229.246° WSW | 38.546° | 2026-08-24 21:38:40.153Z | 339.36° 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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