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 62227U 26145.54830608 +.00000000 +00000-0 +17585-2 0 00002
2 62227 53.1566 82.3318 0001112 96.3869 263.7275 15.69774426 01
| Epoch (UTC): | 25 May 2026 13:09:33 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1566° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 82.3318° |
| argument of perigee: | 96.3869° |
| revolutions per day: | 15.69774426 |
| mean anomaly at epoch: | 263.7275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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