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 32785U 08021C 23336.88030827 .00006714 00000-0 63286-3 0 9995
2 32785 97.7305 299.6180 0009836 263.5140 96.4960 14.94092750846069
| Epoch (UTC): | 02 December 2023 21:07:38 |
| Eccentricity: | 0.0009836 |
| inclination: | 97.7305° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 299.6180° |
| argument of perigee: | 263.5140° |
| revolutions per day: | 14.94092750 |
| mean anomaly at epoch: | 96.4960° |
| orbit number at epoch: | 84606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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