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 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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 IRIDE-MS1-EAG2-13
1 68450U 26067AL 26153.83023876 .00009258 00000-0 45025-3 0 9991
2 68450 97.4542 112.5280 0004019 82.2346 277.9345 15.18620852 9761Epoch: 2026-06-02T19:55Z
TLE epoch observation values (Epoch: 2026-06-02T19:55:32.628Z)
Latitude
0.00001°
Longitude
-77.65553°
Altitude
512.714 km
Speed
7.608 km/s
True Right ascension
07h 30m 06s
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
02:31:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.745 km
Perigee altitude
504.21 km
Semi-major axis
6,885.115 km
Eccentricity
0.0004
Inclination
97.4542°
RAAN
112.528°
Arg. of periapsis
82.2346°
True anomaly
277.88888°
Mean anomaly
277.9345°
Eccentric anomaly
277.91169°
Mean motion
3.79906 °/min
Orbital period
94.76 mins
BSTAR
0.00045025
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-06 20:32:09.380Z | 116.869° SE | 2026-06-06 20:34:09.380Z | 79.362° E | 20.956° | 2026-06-06 20:37:09.380Z | 20.115° NNE |
| 4 mins | 2026-06-06 22:07:09.380Z | 237.696° WSW | 2026-06-06 22:08:09.380Z | 259.616° W | 19.582° | 2026-06-06 22:11:09.380Z | 314.96° NW |
| 5 mins | 2026-06-07 09:37:09.380Z | 42.422° NE | 2026-06-07 09:39:09.380Z | 90.697° ESE | 28.839° | 2026-06-07 09:42:09.380Z | 159.493° S |
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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