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 32791U 08021J 23339.41210584 .00007806 00000-0 63831-3 0 9993
2 32791 97.6822 307.5644 0009362 180.5057 179.6159 14.99592734847373
| Epoch (UTC): | 05 December 2023 09:53:25 |
| Eccentricity: | 0.0009362 |
| inclination: | 97.6822° |
| perigee height: | 561 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 307.5644° |
| argument of perigee: | 180.5057° |
| revolutions per day: | 14.99592734 |
| mean anomaly at epoch: | 179.6159° |
| orbit number at epoch: | 84737 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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