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 07530U 74089B 23332.58637205 -.00000035 00000-0 70015-4 0 9998
2 07530 101.9649 320.4711 0012414 108.6907 6.8994 12.53669654243774
| Epoch (UTC): | 28 November 2023 14:04:22 |
| Eccentricity: | 0.0012414 |
| inclination: | 101.9649° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 320.4711° |
| argument of perigee: | 108.6907° |
| revolutions per day: | 12.53669654 |
| mean anomaly at epoch: | 6.8994° |
| orbit number at epoch: | 24377 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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