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 58U 60013A 22148.77717886 .00000093 00000-0 80059-5 0 9990
2 58 28.3277 90.9452 0165046 190.1227 169.5968 13.46335134 34944
| Epoch (UTC): | 28 May 2022 18:39:08 |
| Eccentricity: | 0.0165046 |
| inclination: | 28.3277° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 90.9452° |
| argument of perigee: | 190.1227° |
| revolutions per day: | 13.46335134 |
| mean anomaly at epoch: | 169.5968° |
| orbit number at epoch: | 3494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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