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 23151.89796920 -.00000240 00000-0 -99627-4 0 9996
2 23088 71.0016 37.4353 0002760 350.9056 9.2016 14.14767586502831
| Epoch (UTC): | 31 May 2023 21:33:04 |
| Eccentricity: | 0.0002760 |
| inclination: | 71.0016° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 37.4353° |
| argument of perigee: | 350.9056° |
| revolutions per day: | 14.14767586 |
| mean anomaly at epoch: | 9.2016° |
| orbit number at epoch: | 50283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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