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 23159.03908719 -.00000173 00000-0 -64807-4 0 9998
2 23088 71.0004 22.4441 0003058 344.8287 15.2743 14.14765173503845
| Epoch (UTC): | 08 June 2023 00:56:17 |
| Eccentricity: | 0.0003058 |
| inclination: | 71.0004° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 22.4441° |
| argument of perigee: | 344.8287° |
| revolutions per day: | 14.14765173 |
| mean anomaly at epoch: | 15.2743° |
| orbit number at epoch: | 50384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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