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 68318U 26145.29336941 +.00000000 +00000-0 +13580-2 0 00003
2 68318 97.2848 271.5381 0000828 81.5702 278.5657 15.75251042 06
| Epoch (UTC): | 25 May 2026 07:02:27 |
| Eccentricity: | 0.0000828 |
| inclination: | 97.2848° |
| perigee height: | 343 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 271.5381° |
| argument of perigee: | 81.5702° |
| revolutions per day: | 15.75251042 |
| mean anomaly at epoch: | 278.5657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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