IRIDE-MS2-HEO-10, 68982
Orbit data source: Space-Track
IRIDE-MS2-HEO-10, 68982 is an Italian payload satellite in SSO that was launched on Sun, 03 May 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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68982 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
ArgoTec
Mission
Operational spacecraft
Bus & Motor
HAWK, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 IRIDE-MS2-HEO-10
1 68982U 26100C 26168.62673606 .00001024 00000-0 10875-3 0 9992
2 68982 97.7336 66.0267 0005071 138.0808 222.0799 14.91157606 6768Epoch: 2026-06-17T15:02Z
TLE epoch observation values (Epoch: 2026-06-17T15:02:29.995Z)
Latitude
-0.00008°
Longitude
-65.47998°
Altitude
599.992 km
Speed
7.558 km/s
True Right ascension
04h 24m 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
12:12:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.878 km
Perigee altitude
587.809 km
Semi-major axis
6,969.48 km
Eccentricity
0.00051
Inclination
97.7336°
RAAN
66.0267°
Arg. of periapsis
138.0808°
True anomaly
222.04098°
Mean anomaly
222.0799°
Eccentric anomaly
222.06044°
Mean motion
3.73029 °/min
Orbital period
96.51 mins
BSTAR
0.00010875
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Other satellites on launch #100 in the year 2026 (2026-05-03 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-MS2-HEO-10 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-18 06:06:00.952Z | 10.764° NNE | 2026-06-18 06:10:00.952Z | 209.081° SW | 43.24° | 2026-06-18 06:13:00.952Z | 195.915° SSW |
| 6 mins | 2026-06-18 16:57:00.952Z | 147.502° SSE | 2026-06-18 17:00:00.952Z | 44.094° NE | 39.284° | 2026-06-18 17:03:00.952Z | 357.525° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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