IRIDE-MS1-EAG2-15, 68462
Orbit data source: Space-Track
IRIDE-MS1-EAG2-15, 68462 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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68462 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: 7 hours ago
TLE from 7 hours ago
0 IRIDE-MS1-EAG2-15
1 68462U 26067AY 26236.57216707 .00006895 00000-0 32844-3 0 9993
2 68462 97.4602 194.1958 0004224 124.3852 235.7783 15.19439023 22321Epoch: 2026-08-24T13:43Z
TLE epoch observation values (Epoch: 2026-08-24T13:43:55.234Z)
Latitude
-0.00001°
Longitude
15.36371°
Altitude
512.26 km
Speed
7.607 km/s
True Right ascension
12h 56m 46s
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
12:10:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.411 km
Perigee altitude
501.597 km
Semi-major axis
6,882.641 km
Eccentricity
0.00042
Inclination
97.4602°
RAAN
194.1958°
Arg. of periapsis
124.3852°
True anomaly
235.73829°
Mean anomaly
235.7783°
Eccentric anomaly
235.75829°
Mean motion
3.80111 °/min
Orbital period
94.71 mins
BSTAR
0.00032844
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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-EAG2-15 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 | 2026-08-24 21:45:28.388Z | 196.097° SSW | 2026-08-24 21:48:28.388Z | 263.974° W | 31.13° | 2026-08-24 21:51:28.388Z | 328.33° NNW |
| 4 mins | 2026-08-25 09:17:28.388Z | 62.89° ENE | 2026-08-25 09:19:28.388Z | 103.995° ESE | 17.544° | 2026-08-25 09:21:28.388Z | 138.273° SSE |
| 4 mins | 2026-08-25 10:51:28.388Z | 324.378° NNW | 2026-08-25 10:52:28.388Z | 301.199° NW | 22.589° | 2026-08-25 10:55:28.388Z | 237.681° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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