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 62022U 26145.33741595 +.00000000 +00000-0 +32204-3 0 00004
2 62022 53.1590 159.5867 0001334 74.6819 285.4329 15.30218939 08
| Epoch (UTC): | 25 May 2026 08:05:52 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.5867° |
| argument of perigee: | 74.6819° |
| revolutions per day: | 15.30218939 |
| mean anomaly at epoch: | 285.4329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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