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 40025U 14033R 23079.62706015 .00006171 00000-0 60116-3 0 9992
2 40025 97.9889 24.9178 0010003 221.0069 139.0398 14.92829061474929
| Epoch (UTC): | 20 March 2023 15:02:57 |
| Eccentricity: | 0.0010003 |
| inclination: | 97.9889° |
| perigee height: | 582 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 24.9178° |
| argument of perigee: | 221.0069° |
| revolutions per day: | 14.92829061 |
| mean anomaly at epoch: | 139.0398° |
| orbit number at epoch: | 47492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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