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 48013C 21024AN 22223.52409722 .00007631 00000-0 51139-3 0 2236
2 48013 53.0542 45.2389 0001264 99.6478 57.5936 15.06384261 16
| Epoch (UTC): | 11 August 2022 12:34:42 |
| Eccentricity: | 0.0001264 |
| inclination: | 53.0542° |
| perigee height: | 546 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 45.2389° |
| argument of perigee: | 99.6478° |
| revolutions per day: | 15.06384261 |
| mean anomaly at epoch: | 57.5936° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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