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 00022U 59009A 23030.86347746 .00003900 00000-0 28841-3 0 9998
2 00022 50.2819 282.6419 0129963 322.7159 36.4821 14.98932099613718
| Epoch (UTC): | 30 January 2023 20:43:24 |
| Eccentricity: | 0.0129963 |
| inclination: | 50.2819° |
| perigee height: | 480 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 282.6419° |
| argument of perigee: | 322.7159° |
| revolutions per day: | 14.98932099 |
| mean anomaly at epoch: | 36.4821° |
| orbit number at epoch: | 61371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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