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 62228U 26145.52377821 +.00000000 +00000-0 +12742-2 0 00004
2 62228 53.1567 82.1704 0001379 74.7695 285.3475 15.69765246 04
| Epoch (UTC): | 25 May 2026 12:34:14 |
| Eccentricity: | 0.0001379 |
| inclination: | 53.1567° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 82.1704° |
| argument of perigee: | 74.7695° |
| revolutions per day: | 15.69765246 |
| mean anomaly at epoch: | 285.3475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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