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 33495U 09002D 23337.64358897 .00001019 00000-0 16657-3 0 9992
2 33495 98.2086 221.2748 0009216 105.0962 255.1265 14.73013835798157
| Epoch (UTC): | 03 December 2023 15:26:46 |
| Eccentricity: | 0.0009216 |
| inclination: | 98.2086° |
| perigee height: | 645 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 221.2748° |
| argument of perigee: | 105.0962° |
| revolutions per day: | 14.73013835 |
| mean anomaly at epoch: | 255.1265° |
| orbit number at epoch: | 79815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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