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 62309U 26145.37486615 +.00000000 +00000-0 +14661-2 0 00001
2 62309 53.1594 185.0217 0001730 15.9490 344.1566 15.31309966 04
| Epoch (UTC): | 25 May 2026 08:59:48 |
| Eccentricity: | 0.0001730 |
| inclination: | 53.1594° |
| perigee height: | 471 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 185.0217° |
| argument of perigee: | 15.9490° |
| revolutions per day: | 15.31309966 |
| mean anomaly at epoch: | 344.1566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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