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 06324U 72104B 23027.82228793 .00000382 00000-0 12009-3 0 9992
2 06324 74.0770 264.9966 0010116 238.9272 121.0893 14.43770052631193
| Epoch (UTC): | 27 January 2023 19:44:05 |
| Eccentricity: | 0.0010116 |
| inclination: | 74.0770° |
| perigee height: | 739 km |
| apogee height: | 753 km |
| right ascension of ascending node: | 264.9966° |
| argument of perigee: | 238.9272° |
| revolutions per day: | 14.43770052 |
| mean anomaly at epoch: | 121.0893° |
| orbit number at epoch: | 63119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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