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 62226U 26145.53849520 +.00000000 +00000-0 +86151-3 0 00009
2 62226 53.1567 82.2671 0001547 80.2454 279.8739 15.69744654 09
| Epoch (UTC): | 25 May 2026 12:55:25 |
| Eccentricity: | 0.0001547 |
| inclination: | 53.1567° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 82.2671° |
| argument of perigee: | 80.2454° |
| revolutions per day: | 15.69744654 |
| mean anomaly at epoch: | 279.8739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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