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 33499U 09002H 23337.10741696 .00002722 00000-0 38643-3 0 9991
2 33499 98.1536 231.4548 0009869 50.6945 309.5139 14.77766515799431
| Epoch (UTC): | 03 December 2023 02:34:40 |
| Eccentricity: | 0.0009869 |
| inclination: | 98.1536° |
| perigee height: | 629 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 231.4548° |
| argument of perigee: | 50.6945° |
| revolutions per day: | 14.77766515 |
| mean anomaly at epoch: | 309.5139° |
| orbit number at epoch: | 79943 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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