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 68499U 26145.32084006 +.00000000 +00000-0 +16168-3 0 00005
2 68499 97.7568 103.8929 0002979 99.8248 260.3307 14.91492635 04
| Epoch (UTC): | 25 May 2026 07:42:00 |
| Eccentricity: | 0.0002979 |
| inclination: | 97.7568° |
| perigee height: | 591 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 103.8929° |
| argument of perigee: | 99.8248° |
| revolutions per day: | 14.91492635 |
| mean anomaly at epoch: | 260.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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