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 62618U 26145.51463684 +.00000000 +00000-0 +11758-2 0 00005
2 62618 97.3958 234.4443 0001553 60.8482 299.2928 15.56815338 08
| Epoch (UTC): | 25 May 2026 12:21:04 |
| Eccentricity: | 0.0001553 |
| inclination: | 97.3958° |
| perigee height: | 396 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 234.4443° |
| argument of perigee: | 60.8482° |
| revolutions per day: | 15.56815338 |
| mean anomaly at epoch: | 299.2928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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