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 23148.07016040 .00002260 00000-0 32147-3 0 9994
2 40012 97.6724 323.1174 0057001 121.0126 239.6700 14.76696305480805
| Epoch (UTC): | 28 May 2023 01:41:01 |
| Eccentricity: | 0.0057001 |
| inclination: | 97.6724° |
| perigee height: | 600 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 323.1174° |
| argument of perigee: | 121.0126° |
| revolutions per day: | 14.76696305 |
| mean anomaly at epoch: | 239.6700° |
| orbit number at epoch: | 48080 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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