IRIDE-MS1-EAG2-16, 68452
Orbit data source: Space-Track
IRIDE-MS1-EAG2-16, 68452 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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68452 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, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 IRIDE-MS1-EAG2-16
1 68452U 26067AN 26174.88543453 .00004825 00000-0 23924-3 0 9998
2 68452 97.4544 133.2090 0005553 58.6782 301.4995 15.18191947 12956Epoch: 2026-06-23T21:15Z
TLE epoch observation values (Epoch: 2026-06-23T21:15:01.543Z)
Latitude
-0.00002°
Longitude
-97.59801°
Altitude
512.394 km
Speed
7.609 km/s
True Right ascension
08h 52m 50s
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
17:55:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.099 km
Perigee altitude
504.451 km
Semi-major axis
6,886.412 km
Eccentricity
0.00056
Inclination
97.4544°
RAAN
133.209°
Arg. of periapsis
58.6782°
True anomaly
301.44522°
Mean anomaly
301.4995°
Eccentric anomaly
301.47236°
Mean motion
3.79799 °/min
Orbital period
94.79 mins
BSTAR
0.00023924
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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-EAG2-16 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 | 2026-06-24 10:28:19.592Z | 353.496° N | 2026-06-24 10:30:19.592Z | 311.371° NW | 34.595° | 2026-06-24 10:34:19.592Z | 212.119° SW |
| 5 mins | 2026-06-24 21:07:19.592Z | 151.281° SSE | 2026-06-24 21:09:19.592Z | 82.291° E | 42.017° | 2026-06-24 21:12:19.592Z | 356.213° 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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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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