IRIDE-MS1-EAG2-9, 68449
Orbit data source: Space-Track
IRIDE-MS1-EAG2-9, 68449 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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68449 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: 12 hours ago
TLE from 12 hours ago
0 IRIDE-MS1-EAG2-9
1 68449U 26067AK 26254.42269704 .00005742 00000-0 27756-3 0 9993
2 68449 97.4597 211.5895 0005741 114.4321 245.7513 15.18995515 25023Epoch: 2026-09-11T10:08Z
TLE epoch observation values (Epoch: 2026-09-11T10:08:41.024Z)
Latitude
0°
Longitude
68.97229°
Altitude
513.589 km
Speed
7.606 km/s
True Right ascension
14h 06m 21s
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
14:42:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.797 km
Perigee altitude
501.892 km
Semi-major axis
6,883.982 km
Eccentricity
0.00057
Inclination
97.4597°
RAAN
211.5895°
Arg. of periapsis
114.4321°
True anomaly
245.69133°
Mean anomaly
245.7513°
Eccentric anomaly
245.72132°
Mean motion
3.8 °/min
Orbital period
94.74 mins
BSTAR
0.00027756
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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-EAG2-9 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 | 2026-09-12 10:25:08.651Z | 358.605° N | 2026-09-12 10:28:08.651Z | 284.37° WNW | 50.649° | 2026-09-12 10:31:08.651Z | 212.029° SW |
| 5 mins | 2026-09-12 21:04:08.651Z | 147.875° SSE | 2026-09-12 21:06:08.651Z | 90.277° ESE | 57.487° | 2026-09-12 21:09:08.651Z | 359.035° 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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