IRIDE-MS2-HEO-15, 68987
Orbit data source: Space-Track
IRIDE-MS2-HEO-15, 68987 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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68987 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-15
1 68987U 26100H 26168.67679880 .00001246 00000-0 12902-3 0 9991
2 68987 97.7339 66.1157 0002906 107.9406 252.2130 14.91806726 6777Epoch: 2026-06-17T16:14Z
TLE epoch observation values (Epoch: 2026-06-17T16:14:35.416Z)
Latitude
0°
Longitude
-83.46292°
Altitude
595.964 km
Speed
7.561 km/s
True Right ascension
04h 24m 27s
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
12:49:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.344 km
Perigee altitude
587.295 km
Semi-major axis
6,967.457 km
Eccentricity
0.00029
Inclination
97.7339°
RAAN
66.1157°
Arg. of periapsis
107.9406°
True anomaly
252.1813°
Mean anomaly
252.213°
Eccentric anomaly
252.19715°
Mean motion
3.73192 °/min
Orbital period
96.47 mins
BSTAR
0.00012902
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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-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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-18 05:41:33.727Z | 27.111° NE | 2026-06-18 05:44:33.727Z | 81.367° E | 35.957° | 2026-06-18 05:48:33.727Z | 173.062° S |
| 5 mins | 2026-06-18 16:32:33.727Z | 118.369° SE | 2026-06-18 16:34:33.727Z | 76.385° E | 26.585° | 2026-06-18 16:37:33.727Z | 16.058° NNE |
| 4 mins | 2026-06-18 18:08:33.727Z | 232.821° WSW | 2026-06-18 18:10:33.727Z | 270.155° WNW | 19.182° | 2026-06-18 18:12:33.727Z | 304.596° NW |
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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