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 62218U 26145.55321065 +.00000000 +00000-0 +14302-2 0 00009
2 62218 53.1568 82.3697 0001094 97.7712 262.3430 15.69762010 08
| Epoch (UTC): | 25 May 2026 13:16:37 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1568° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 82.3697° |
| argument of perigee: | 97.7712° |
| revolutions per day: | 15.69762010 |
| mean anomaly at epoch: | 262.3430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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