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 42789U 17036AA 23088.85408217 .00059047 00000-0 13060-2 0 9990
2 42789 97.1593 129.3162 0006584 34.1217 326.0454 15.43598623320848
| Epoch (UTC): | 29 March 2023 20:29:52 |
| Eccentricity: | 0.0006584 |
| inclination: | 97.1593° |
| perigee height: | 431 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 129.3162° |
| argument of perigee: | 34.1217° |
| revolutions per day: | 15.43598623 |
| mean anomaly at epoch: | 326.0454° |
| orbit number at epoch: | 32084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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