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 36799U 10035E 23083.86095033 .00010718 00000-0 97671-3 0 9993
2 36799 98.1493 310.1937 0009904 252.0557 107.9583 14.95293423689820
| Epoch (UTC): | 24 March 2023 20:39:46 |
| Eccentricity: | 0.0009904 |
| inclination: | 98.1493° |
| perigee height: | 574 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 310.1937° |
| argument of perigee: | 252.0557° |
| revolutions per day: | 14.95293423 |
| mean anomaly at epoch: | 107.9583° |
| orbit number at epoch: | 68982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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