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 62386U 26145.46503552 +.00000000 +00000-0 +21020-3 0 00004
2 62386 44.9837 57.4233 0004596 267.1963 92.8395 15.28807526 04
| Epoch (UTC): | 25 May 2026 11:09:39 |
| Eccentricity: | 0.0004596 |
| inclination: | 44.9837° |
| perigee height: | 476 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 57.4233° |
| argument of perigee: | 267.1963° |
| revolutions per day: | 15.28807526 |
| mean anomaly at epoch: | 92.8395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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