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 33244U 08036A 23072.77298807 0.00000000 00000-0 00000-0 0 08
2 33244 98.1968 119.6369 0000493 19.9431 340.0135 15.28760681 07
| Epoch (UTC): | 13 March 2023 18:33:06 |
| Eccentricity: | 0.0000493 |
| inclination: | 98.1968° |
| perigee height: | 479 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 119.6369° |
| argument of perigee: | 19.9431° |
| revolutions per day: | 15.28760681 |
| mean anomaly at epoch: | 340.0135° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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