IRIDE-MS1-EAG2-14, 68447
Orbit data source: Space-Track
IRIDE-MS1-EAG2-14, 68447 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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68447 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: 9 hours ago
TLE from 9 hours ago
0 IRIDE-MS1-EAG2-14
1 68447U 26067AH 26263.14647853 .00005200 00000-0 24400-3 0 9997
2 68447 97.4616 220.4595 0003281 67.5364 292.6218 15.20083717 26367Epoch: 2026-09-20T03:30Z
TLE epoch observation values (Epoch: 2026-09-20T03:30:55.744Z)
Latitude
-0.00008°
Longitude
168.6824°
Altitude
507.808 km
Speed
7.611 km/s
True Right ascension
14h 41m 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
05:11:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.814 km
Perigee altitude
500.298 km
Semi-major axis
6,880.693 km
Eccentricity
0.00033
Inclination
97.4616°
RAAN
220.4595°
Arg. of periapsis
67.5364°
True anomaly
292.58709°
Mean anomaly
292.6218°
Eccentric anomaly
292.60445°
Mean motion
3.80272 °/min
Orbital period
94.67 mins
BSTAR
0.000244
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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-EAG2-14 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 | 2026-09-20 21:01:43.449Z | 147.516° SSE | 2026-09-20 21:04:43.449Z | 53.232° ENE | 50.692° | 2026-09-20 21:07:43.449Z | 358.989° N |
| 5 mins | 2026-09-21 10:06:43.449Z | 15.203° NNE | 2026-09-21 10:08:43.449Z | 91.315° ESE | 83.71° | 2026-09-21 10:11:43.449Z | 190.338° SSW |
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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