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 62223U 26145.52868727 +.00000000 +00000-0 +16246-2 0 00002
2 62223 53.1563 82.2047 0001994 77.1568 282.9672 15.69767560 08
| Epoch (UTC): | 25 May 2026 12:41:18 |
| Eccentricity: | 0.0001994 |
| inclination: | 53.1563° |
| perigee height: | 358 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 82.2047° |
| argument of perigee: | 77.1568° |
| revolutions per day: | 15.69767560 |
| mean anomaly at epoch: | 282.9672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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