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 23159.05148556 .00000310 00000-0 98564-4 0 9993
2 06324 74.0785 21.6228 0009471 313.9900 46.0476 14.43937481650131
| Epoch (UTC): | 08 June 2023 01:14:08 |
| Eccentricity: | 0.0009471 |
| inclination: | 74.0785° |
| perigee height: | 739 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 21.6228° |
| argument of perigee: | 313.9900° |
| revolutions per day: | 14.43937481 |
| mean anomaly at epoch: | 46.0476° |
| orbit number at epoch: | 65013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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