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 23030.13013182 .00004576 00000-0 33457-3 0 9991
2 22 50.2819 286.1029 0129987 319.8959 39.2449 14.98925409368569
| Epoch (UTC): | 30 January 2023 03:07:23 |
| Eccentricity: | 0.0129987 |
| inclination: | 50.2819° |
| perigee height: | 480 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 286.1029° |
| argument of perigee: | 319.8959° |
| revolutions per day: | 14.98925409 |
| mean anomaly at epoch: | 39.2449° |
| orbit number at epoch: | 36856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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