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 35500U 09036C 23088.46588976 .00000017 00000-0 50171-4 0 9991
2 35500 82.4842 98.2859 0006655 195.2903 164.7976 12.41480384622213
| Epoch (UTC): | 29 March 2023 11:10:52 |
| Eccentricity: | 0.0006655 |
| inclination: | 82.4842° |
| perigee height: | 1495 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 98.2859° |
| argument of perigee: | 195.2903° |
| revolutions per day: | 12.41480384 |
| mean anomaly at epoch: | 164.7976° |
| orbit number at epoch: | 62221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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