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 68202U 26145.62629837 +.00000000 +00000-0 +38547-3 0 00002
2 68202 97.5328 220.8016 0012063 37.0662 323.1399 15.11098326 05
| Epoch (UTC): | 25 May 2026 15:01:52 |
| Eccentricity: | 0.0012063 |
| inclination: | 97.5328° |
| perigee height: | 525 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 220.8016° |
| argument of perigee: | 37.0662° |
| revolutions per day: | 15.11098326 |
| mean anomaly at epoch: | 323.1399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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