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 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-EAG2-16
1 68452U 26067AN 26234.85106254 .00006035 00000-0 29311-3 0 9997
2 68452 97.4595 192.3539 0004218 159.8036 200.3365 15.18816835 22059Epoch: 2026-08-22T20:25Z
TLE epoch observation values (Epoch: 2026-08-22T20:25:31.803Z)
Latitude
-0.00012°
Longitude
-85.18414°
Altitude
515.227 km
Speed
7.605 km/s
True Right ascension
12h 49m 24s
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
20:03:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.289 km
Perigee altitude
503.481 km
Semi-major axis
6,884.522 km
Eccentricity
0.00042
Inclination
97.4595°
RAAN
192.3539°
Arg. of periapsis
159.8036°
True anomaly
200.31971°
Mean anomaly
200.3365°
Eccentric anomaly
200.3281°
Mean motion
3.79955 °/min
Orbital period
94.75 mins
BSTAR
0.00029311
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-24 09:21:57.197Z | 44.409° NE | 2026-08-24 09:24:57.197Z | 102.058° ESE | 20.637° | 2026-08-24 09:26:57.197Z | 140.794° SSE |
| 4 mins | 2026-08-24 10:56:57.197Z | 324.114° NNW | 2026-08-24 10:58:57.197Z | 279.572° WNW | 19.741° | 2026-08-24 11:00:57.197Z | 243.952° WSW |
| 5 mins | 2026-08-24 21:34:57.197Z | 192.322° SSW | 2026-08-24 21:36:57.197Z | 260.537° W | 38.472° | 2026-08-24 21:39:57.197Z | 335.31° 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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