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 6324U 72104B 23151.15318708 .00000278 00000-0 89065-4 0 9993
2 6324 74.0791 36.2724 0009275 329.3212 30.7401 14.43932031649266
| Epoch (UTC): | 31 May 2023 03:40:35 |
| Eccentricity: | 0.0009275 |
| inclination: | 74.0791° |
| perigee height: | 739 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 36.2724° |
| argument of perigee: | 329.3212° |
| revolutions per day: | 14.43932031 |
| mean anomaly at epoch: | 30.7401° |
| orbit number at epoch: | 64926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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