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 23092.14403118 .00006403 00000-0 64232-3 0 9997
2 32785 97.6983 59.7972 0012508 5.7958 354.3403 14.91602790809556
| Epoch (UTC): | 02 April 2023 03:27:24 |
| Eccentricity: | 0.0012508 |
| inclination: | 97.6983° |
| perigee height: | 584 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 59.7972° |
| argument of perigee: | 5.7958° |
| revolutions per day: | 14.91602790 |
| mean anomaly at epoch: | 354.3403° |
| orbit number at epoch: | 80955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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