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 23156.62657266 .00000282 00000-0 90199-4 0 9990
2 06324 74.0786 26.1206 0009392 318.7193 41.3253 14.43935597649783
| Epoch (UTC): | 05 June 2023 15:02:15 |
| Eccentricity: | 0.0009392 |
| inclination: | 74.0786° |
| perigee height: | 739 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 26.1206° |
| argument of perigee: | 318.7193° |
| revolutions per day: | 14.43935597 |
| mean anomaly at epoch: | 41.3253° |
| orbit number at epoch: | 64978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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