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 68382U 26145.40099865 +.00000000 +00000-0 +86834-3 0 00001
2 68382 97.2854 287.9945 0001435 96.8598 263.2808 15.33454061 07
| Epoch (UTC): | 25 May 2026 09:37:26 |
| Eccentricity: | 0.0001435 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.9945° |
| argument of perigee: | 96.8598° |
| revolutions per day: | 15.33454061 |
| mean anomaly at epoch: | 263.2808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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