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 36508U 10013A 22222.83791421 .00000060 00000-0 14250-4 0 9994
2 36508 92.0356 297.3025 0006919 72.8646 287.3319 14.51896235654029
| Epoch (UTC): | 10 August 2022 20:06:35 |
| Eccentricity: | 0.0006919 |
| inclination: | 92.0356° |
| perigee height: | 714 km |
| apogee height: | 724 km |
| right ascension of ascending node: | 297.3025° |
| argument of perigee: | 72.8646° |
| revolutions per day: | 14.51896235 |
| mean anomaly at epoch: | 287.3319° |
| orbit number at epoch: | 65402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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