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 40012U 14033C 23087.95821107 .00003932 00000-0 56086-3 0 9996
2 40012 97.6688 266.0063 0055149 317.5807 42.1147 14.76255162471933
| Epoch (UTC): | 28 March 2023 22:59:49 |
| Eccentricity: | 0.0055149 |
| inclination: | 97.6688° |
| perigee height: | 602 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 266.0063° |
| argument of perigee: | 317.5807° |
| revolutions per day: | 14.76255162 |
| mean anomaly at epoch: | 42.1147° |
| orbit number at epoch: | 47193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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