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 68083U 26145.38719036 +.00000000 +00000-0 +43338-3 0 00007
2 68083 53.1585 182.0737 0001026 79.1731 280.9387 15.34373962 09
| Epoch (UTC): | 25 May 2026 09:17:33 |
| Eccentricity: | 0.0001026 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 182.0737° |
| argument of perigee: | 79.1731° |
| revolutions per day: | 15.34373962 |
| mean anomaly at epoch: | 280.9387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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