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 62222U 26145.24467366 +.00000000 +00000-0 +13912-2 0 00001
2 62222 53.1570 84.0002 0000964 87.4412 272.6716 15.69771342 02
| Epoch (UTC): | 25 May 2026 05:52:19 |
| Eccentricity: | 0.0000964 |
| inclination: | 53.1570° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 84.0002° |
| argument of perigee: | 87.4412° |
| revolutions per day: | 15.69771342 |
| mean anomaly at epoch: | 272.6716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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