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 62968U 26145.52248356 +.00000000 +00000-0 +47273-3 0 00003
2 62968 53.1589 235.3912 0001054 90.2513 269.8609 15.31712671 03
| Epoch (UTC): | 25 May 2026 12:32:22 |
| Eccentricity: | 0.0001054 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.3912° |
| argument of perigee: | 90.2513° |
| revolutions per day: | 15.31712671 |
| mean anomaly at epoch: | 269.8609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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