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 68913U 26145.43276508 +.00000000 +00000-0 +10598-2 0 00008
2 68913 97.2854 341.1907 0002699 77.4649 282.6904 15.49234582 06
| Epoch (UTC): | 25 May 2026 10:23:10 |
| Eccentricity: | 0.0002699 |
| inclination: | 97.2854° |
| perigee height: | 417 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 341.1907° |
| argument of perigee: | 77.4649° |
| revolutions per day: | 15.49234582 |
| mean anomaly at epoch: | 282.6904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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