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 36582U 10021B 22338.25412788 .00000097 00000-0 00000-0 0 9999
2 36582 0.0489 107.3758 0003047 159.7953 270.5497 1.00271104 46012
| Epoch (UTC): | 04 December 2022 06:05:56 |
| Eccentricity: | 0.0003047 |
| inclination: | 0.0489° |
| perigee height: | 35773 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 107.3758° |
| argument of perigee: | 159.7953° |
| revolutions per day: | 1.00271104 |
| mean anomaly at epoch: | 270.5497° |
| orbit number at epoch: | 4601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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