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 38773U 12048P 22223.90872491 0.00000000 00000-0 00000-0 0 07
2 38773 63.4294 191.1439 0187069 359.3344 0.6656 13.40833418 06
| Epoch (UTC): | 11 August 2022 21:48:33 |
| Eccentricity: | 0.0187069 |
| inclination: | 63.4294° |
| perigee height: | 966 km |
| apogee height: | 1246 km |
| right ascension of ascending node: | 191.1439° |
| argument of perigee: | 359.3344° |
| revolutions per day: | 13.40833418 |
| mean anomaly at epoch: | 0.6656° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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