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 22220U 92076B 24282.55385503 .00000736 00000-0 39152-3 0 9993
2 22220 71.0008 197.6086 0012393 173.5280 358.5623 14.16713841648586
| Epoch (UTC): | 08 October 2024 13:17:33 |
| Eccentricity: | 0.0012393 |
| inclination: | 71.0008° |
| perigee height: | 827 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 197.6086° |
| argument of perigee: | 173.5280° |
| revolutions per day: | 14.16713841 |
| mean anomaly at epoch: | 358.5623° |
| orbit number at epoch: | 64858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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