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 68635U 26145.33967730 +.00000000 +00000-0 +46005-3 0 00005
2 68635 60.0227 265.7946 0025924 6.9371 353.2063 15.24774121 00
| Epoch (UTC): | 25 May 2026 08:09:08 |
| Eccentricity: | 0.0025924 |
| inclination: | 60.0227° |
| perigee height: | 474 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 265.7946° |
| argument of perigee: | 6.9371° |
| revolutions per day: | 15.24774121 |
| mean anomaly at epoch: | 353.2063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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