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 00979U 65004B 22331.69739817 .00000174 00000-0 23440-3 0 9999
2 00979 96.4332 71.7217 1142233 205.8187 148.1350 12.14800986557970
| Epoch (UTC): | 27 November 2022 16:44:15 |
| Eccentricity: | 0.1142233 |
| inclination: | 96.4332° |
| perigee height: | 702 km |
| apogee height: | 2528 km |
| right ascension of ascending node: | 71.7217° |
| argument of perigee: | 205.8187° |
| revolutions per day: | 12.14800986 |
| mean anomaly at epoch: | 148.1350° |
| orbit number at epoch: | 55797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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