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 33493U 09002B 23080.25575275 .00014746 00000-0 10602-2 0 9997
2 33493 98.2492 88.7326 0016092 347.6147 12.4679 15.04264982770523
| Epoch (UTC): | 21 March 2023 06:08:17 |
| Eccentricity: | 0.0016092 |
| inclination: | 98.2492° |
| perigee height: | 542 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 88.7326° |
| argument of perigee: | 347.6147° |
| revolutions per day: | 15.04264982 |
| mean anomaly at epoch: | 12.4679° |
| orbit number at epoch: | 77052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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