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 39369U 13055AC 23336.83149033 .00074104 17702-6 82532-3 0 9994
2 39369 80.9532 270.4721 0289581 93.8507 269.5882 15.25435494534191
| Epoch (UTC): | 02 December 2023 19:57:20 |
| Eccentricity: | 0.0289581 |
| inclination: | 80.9532° |
| perigee height: | 290 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 270.4721° |
| argument of perigee: | 93.8507° |
| revolutions per day: | 15.25435494 |
| mean anomaly at epoch: | 269.5882° |
| orbit number at epoch: | 53419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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