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 32706U 08010A 23059.55927073 0.00000000 00000-0 00000-0 0 07
2 32706 63.6908 112.1802 6920083 268.1360 91.8637 2.00612210 09
| Epoch (UTC): | 28 February 2023 13:25:20 |
| Eccentricity: | 0.6920083 |
| inclination: | 63.6908° |
| perigee height: | 1801 km |
| apogee height: | 38554 km |
| right ascension of ascending node: | 112.1802° |
| argument of perigee: | 268.1360° |
| revolutions per day: | 2.00612210 |
| mean anomaly at epoch: | 91.8637° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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