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 23081.04452146 .00003375 00000-0 48293-3 0 9995
2 40012 97.6670 259.4422 0055606 340.2819 19.6241 14.76194002470919
| Epoch (UTC): | 22 March 2023 01:04:06 |
| Eccentricity: | 0.0055606 |
| inclination: | 97.6670° |
| perigee height: | 602 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 259.4422° |
| argument of perigee: | 340.2819° |
| revolutions per day: | 14.76194002 |
| mean anomaly at epoch: | 19.6241° |
| orbit number at epoch: | 47091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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