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 21065.69306860 .00000085 00000-0 36516-5 0 9994
2 00058 28.3258 204.2181 0165022 80.3388 281.5757 13.46325573973987
| Epoch (UTC): | 06 March 2021 16:38:01 |
| Eccentricity: | 0.0165022 |
| inclination: | 28.3258° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 204.2181° |
| argument of perigee: | 80.3388° |
| revolutions per day: | 13.46325573 |
| mean anomaly at epoch: | 281.5757° |
| orbit number at epoch: | 97398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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