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 23788U 96009B 23088.15954047 .00000030 00000-0 10911-3 0 9996
2 23788 82.5735 336.9472 0006024 211.2282 148.8452 12.63169653249610
| Epoch (UTC): | 29 March 2023 03:49:44 |
| Eccentricity: | 0.0006024 |
| inclination: | 82.5735° |
| perigee height: | 1405 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 336.9472° |
| argument of perigee: | 211.2282° |
| revolutions per day: | 12.63169653 |
| mean anomaly at epoch: | 148.8452° |
| orbit number at epoch: | 24961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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