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 22141.92351655 .00009348 00000-0 76297-3 0 9997
2 33493 98.2335 126.9888 0011891 250.3855 109.6083 14.99613960725003
| Epoch (UTC): | 21 May 2022 22:09:51 |
| Eccentricity: | 0.0011891 |
| inclination: | 98.2335° |
| perigee height: | 560 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 126.9888° |
| argument of perigee: | 250.3855° |
| revolutions per day: | 14.99613960 |
| mean anomaly at epoch: | 109.6083° |
| orbit number at epoch: | 72500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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