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 68854U 26145.58335647 +.00000000 +00000-0 +48302-3 0 00003
2 68854 97.2853 160.3556 0001230 89.7427 314.7058 15.49179389 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001230 |
| inclination: | 97.2853° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.3556° |
| argument of perigee: | 89.7427° |
| revolutions per day: | 15.49179389 |
| mean anomaly at epoch: | 314.7058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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