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 23152.95853031 -.00000241 00000-0 -10037-3 0 9999
2 23088 71.0014 35.2090 0002797 350.0519 10.0548 14.14767237502987
| Epoch (UTC): | 01 June 2023 23:00:17 |
| Eccentricity: | 0.0002797 |
| inclination: | 71.0014° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 35.2090° |
| argument of perigee: | 350.0519° |
| revolutions per day: | 14.14767237 |
| mean anomaly at epoch: | 10.0548° |
| orbit number at epoch: | 50298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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