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 00058U 60013A 22219.36741468 .00000081 00000-0 -15291-5 0 9991
2 00058 28.3274 92.8203 0164874 54.5742 307.0079 13.46336292 43925
| Epoch (UTC): | 07 August 2022 08:49:04 |
| Eccentricity: | 0.0164874 |
| inclination: | 28.3274° |
| perigee height: | 963 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 92.8203° |
| argument of perigee: | 54.5742° |
| revolutions per day: | 13.46336292 |
| mean anomaly at epoch: | 307.0079° |
| orbit number at epoch: | 4392 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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