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 31620U 99025CAA 24357.98503159 .00012948 00000-0 49571-2 0 9990
2 31620 98.9039 65.9410 0021802 1.5055 358.6188 14.30592190908433
| Epoch (UTC): | 22 December 2024 23:38:26 |
| Eccentricity: | 0.0021802 |
| inclination: | 98.9039° |
| perigee height: | 774 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 65.9410° |
| argument of perigee: | 1.5055° |
| revolutions per day: | 14.30592190 |
| mean anomaly at epoch: | 358.6188° |
| orbit number at epoch: | 90843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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