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 31708U 07027C 22225.08917291 0.00000000 00000-0 00000-0 0 08
2 31708 63.3957 318.4757 0355080 20.9507 338.9432 13.40817044 07
| Epoch (UTC): | 13 August 2022 02:08:24 |
| Eccentricity: | 0.0355080 |
| inclination: | 63.3957° |
| perigee height: | 840 km |
| apogee height: | 1372 km |
| right ascension of ascending node: | 318.4757° |
| argument of perigee: | 20.9507° |
| revolutions per day: | 13.40817044 |
| mean anomaly at epoch: | 338.9432° |
| 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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