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 04221U 69097A 22220.87592122 .00014979 00000-0 63074-3 0 9997
2 04221 102.7052 254.9689 0576421 69.9335 296.2912 14.37949018517382
| Epoch (UTC): | 08 August 2022 21:01:19 |
| Eccentricity: | 0.0576421 |
| inclination: | 102.7052° |
| perigee height: | 353 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 254.9689° |
| argument of perigee: | 69.9335° |
| revolutions per day: | 14.37949018 |
| mean anomaly at epoch: | 296.2912° |
| orbit number at epoch: | 51738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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