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 62301U 26145.51554845 +.00000000 +00000-0 +53879-3 0 00005
2 62301 53.1588 184.4804 0001071 89.1486 270.9637 15.30199727 06
| Epoch (UTC): | 25 May 2026 12:22:23 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.4804° |
| argument of perigee: | 89.1486° |
| revolutions per day: | 15.30199727 |
| mean anomaly at epoch: | 270.9637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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