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 51081U 22002DB 23032.12690924 .00015012 00000-0 66581-3 0 9992
2 51081 97.4805 103.0823 0012805 22.0590 338.1194 15.21615061 58157
| Epoch (UTC): | 01 February 2023 03:02:44 |
| Eccentricity: | 0.0012805 |
| inclination: | 97.4805° |
| perigee height: | 492 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 103.0823° |
| argument of perigee: | 22.0590° |
| revolutions per day: | 15.21615061 |
| mean anomaly at epoch: | 338.1194° |
| orbit number at epoch: | 5815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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