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 36447U 93036BAW 22175.80065171 .00016903 00000-0 97829-3 0 9997
2 36447 73.9284 340.3809 0064229 194.7756 165.1562 15.10454185689090
| Epoch (UTC): | 24 June 2022 19:12:56 |
| Eccentricity: | 0.0064229 |
| inclination: | 73.9284° |
| perigee height: | 490 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 340.3809° |
| argument of perigee: | 194.7756° |
| revolutions per day: | 15.10454185 |
| mean anomaly at epoch: | 165.1562° |
| orbit number at epoch: | 68909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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