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 68983U 26145.47484821 +.00000000 +00000-0 +13998-3 0 00006
2 68983 97.7406 43.3442 0002848 193.8204 166.2937 14.91297835 01
| Epoch (UTC): | 25 May 2026 11:23:46 |
| Eccentricity: | 0.0002848 |
| inclination: | 97.7406° |
| perigee height: | 592 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 43.3442° |
| argument of perigee: | 193.8204° |
| revolutions per day: | 14.91297835 |
| mean anomaly at epoch: | 166.2937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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