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 data is extracted from the following two-line orbital elements,
1 22U 59009A 23150.79498898 .00007496 00000-0 51376-3 0 9991
2 22 50.2805 75.8389 0126904 64.4034 296.9968 15.00632602386673
| Epoch (UTC): | 30 May 2023 19:04:47 |
| Eccentricity: | 0.0126904 |
| inclination: | 50.2805° |
| perigee height: | 477 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 75.8389° |
| argument of perigee: | 64.4034° |
| revolutions per day: | 15.00632602 |
| mean anomaly at epoch: | 296.9968° |
| orbit number at epoch: | 38667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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