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 36104U 09066A 23092.83699703 0.00003761 00000-0 33928-3 0 04
2 36104 97.4334 128.0380 0004418 278.3653 81.5313 14.95599196 08
| Epoch (UTC): | 02 April 2023 20:05:16 |
| Eccentricity: | 0.0004418 |
| inclination: | 97.4334° |
| perigee height: | 577 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 128.0380° |
| argument of perigee: | 278.3653° |
| revolutions per day: | 14.95599196 |
| mean anomaly at epoch: | 81.5313° |
| 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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