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 23081.04354861 -.00000190 00000-0 00000+0 0 9995
2 23589 11.2787 15.9498 0005082 19.5815 164.2145 0.98753053101303
| Epoch (UTC): | 22 March 2023 01:02:42 |
| Eccentricity: | 0.0005082 |
| inclination: | 11.2787° |
| perigee height: | 36196 km |
| apogee height: | 36239 km |
| right ascension of ascending node: | 15.9498° |
| argument of perigee: | 19.5815° |
| revolutions per day: | 0.98753053 |
| mean anomaly at epoch: | 164.2145° |
| orbit number at epoch: | 10130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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