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 23088U 94023B 23156.63514494 -.00000239 00000-0 -99314-4 0 9998
2 23088 71.0007 27.4907 0002973 346.6598 13.4445 14.14765782503508
| Epoch (UTC): | 05 June 2023 15:14:36 |
| Eccentricity: | 0.0002973 |
| inclination: | 71.0007° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 27.4907° |
| argument of perigee: | 346.6598° |
| revolutions per day: | 14.14765782 |
| mean anomaly at epoch: | 13.4445° |
| orbit number at epoch: | 50350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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