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 36002U 93036AWU 23340.77927190 .00011477 00000-0 12740-2 0 9992
2 36002 74.0099 14.7497 0060574 334.1563 25.6592 14.85944647775674
| Epoch (UTC): | 06 December 2023 18:42:09 |
| Eccentricity: | 0.0060574 |
| inclination: | 74.0099° |
| perigee height: | 568 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 14.7497° |
| argument of perigee: | 334.1563° |
| revolutions per day: | 14.85944647 |
| mean anomaly at epoch: | 25.6592° |
| orbit number at epoch: | 77567 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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