IRIDE-MS2-HEO-12, 68984
Orbit data source: Space-Track
IRIDE-MS2-HEO-12, 68984 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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68984 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-12
1 68984U 26100E 26168.62877963 .00001029 00000-0 10920-3 0 9992
2 68984 97.7342 66.0269 0005073 136.4196 223.7424 14.91169926 6764Epoch: 2026-06-17T15:05Z
TLE epoch observation values (Epoch: 2026-06-17T15:05:26.560Z)
Latitude
0°
Longitude
-66.21749°
Altitude
599.885 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
12:09:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.841 km
Perigee altitude
587.769 km
Semi-major axis
6,969.442 km
Eccentricity
0.00051
Inclination
97.7342°
RAAN
66.0269°
Arg. of periapsis
136.4196°
True anomaly
223.70222°
Mean anomaly
223.7424°
Eccentric anomaly
223.72231°
Mean motion
3.73032 °/min
Orbital period
96.51 mins
BSTAR
0.0001092
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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-12 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-18 06:08:20.695Z | 9.437° NNE | 2026-06-18 06:12:20.695Z | 308.319° NW | 44.256° | 2026-06-18 06:16:20.695Z | 198.294° SSW |
| 6 mins | 2026-06-18 17:00:20.695Z | 148.26° SSE | 2026-06-18 17:02:20.695Z | 84.738° E | 41.871° | 2026-06-18 17:06:20.695Z | 354.658° 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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