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 24753U 97012A 23156.69687460 .00000080 00000-0 63124-4 0 9991
2 24753 98.9093 197.3091 0008926 18.4866 341.6631 14.16118911351768
| Epoch (UTC): | 05 June 2023 16:43:29 |
| Eccentricity: | 0.0008926 |
| inclination: | 98.9093° |
| perigee height: | 832 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 197.3091° |
| argument of perigee: | 18.4866° |
| revolutions per day: | 14.16118911 |
| mean anomaly at epoch: | 341.6631° |
| orbit number at epoch: | 35176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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