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 62220U 26145.24957472 +.00000000 +00000-0 +19703-2 0 00005
2 62220 53.1564 84.0346 0001034 101.5905 258.5229 15.69812448 03
| Epoch (UTC): | 25 May 2026 05:59:23 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.1564° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 84.0346° |
| argument of perigee: | 101.5905° |
| revolutions per day: | 15.69812448 |
| mean anomaly at epoch: | 258.5229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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