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 22913U 93073C 24357.85941013 .00147585 -53843-5 19193-2 0 9995
2 22913 6.7403 268.1585 2412773 152.4358 222.7522 10.68019617650033
| Epoch (UTC): | 22 December 2024 20:37:33 |
| Eccentricity: | 0.2412773 |
| inclination: | 6.7403° |
| perigee height: | 230 km |
| apogee height: | 4433 km |
| right ascension of ascending node: | 268.1585° |
| argument of perigee: | 152.4358° |
| revolutions per day: | 10.68019617 |
| mean anomaly at epoch: | 222.7522° |
| orbit number at epoch: | 65003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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