View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68915U 26145.58335647 +.00000000 +00000-0 -49823-1 0 00009
2 68915 97.2847 341.4493 0001752 90.8310 276.1401 15.49081781 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001752 |
| inclination: | 97.2847° |
| perigee height: | 418 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 341.4493° |
| argument of perigee: | 90.8310° |
| revolutions per day: | 15.49081781 |
| mean anomaly at epoch: | 276.1401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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