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 62422U 26145.33709816 +.00000000 +00000-0 +88072-3 0 00002
2 62422 43.0018 249.1767 0001118 272.5486 87.5237 15.27590132 02
| Epoch (UTC): | 25 May 2026 08:05:25 |
| Eccentricity: | 0.0001118 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 249.1767° |
| argument of perigee: | 272.5486° |
| revolutions per day: | 15.27590132 |
| mean anomaly at epoch: | 87.5237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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