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 23154.13237337 .00000325 00000-0 10294-3 0 9992
2 06324 74.0789 30.7468 0009329 323.5742 36.4780 14.43934136649420
| Epoch (UTC): | 03 June 2023 03:10:37 |
| Eccentricity: | 0.0009329 |
| inclination: | 74.0789° |
| perigee height: | 739 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 30.7468° |
| argument of perigee: | 323.5742° |
| revolutions per day: | 14.43934136 |
| mean anomaly at epoch: | 36.4780° |
| orbit number at epoch: | 64942 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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