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 23589U 95027A 21105.56728925 -.00000023 00000-0 00000-0 0 9999
2 23589 10.9110 19.2586 0007735 4.1064 293.5609 0.98749122 94345
| Epoch (UTC): | 15 April 2021 13:36:53 |
| Eccentricity: | 0.0007735 |
| inclination: | 10.9110° |
| perigee height: | 36185 km |
| apogee height: | 36251 km |
| right ascension of ascending node: | 19.2586° |
| argument of perigee: | 4.1064° |
| revolutions per day: | 0.98749122 |
| mean anomaly at epoch: | 293.5609° |
| orbit number at epoch: | 9434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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