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 39161U 13021C 23079.43623270 .00003350 00000-0 51813-3 0 9997
2 39161 97.8787 154.2213 0008225 253.2678 106.7590 14.73888186530107
| Epoch (UTC): | 20 March 2023 10:28:10 |
| Eccentricity: | 0.0008225 |
| inclination: | 97.8787° |
| perigee height: | 643 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 154.2213° |
| argument of perigee: | 253.2678° |
| revolutions per day: | 14.73888186 |
| mean anomaly at epoch: | 106.7590° |
| orbit number at epoch: | 53010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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