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 23089.04755761 .00000130 00000-0 63728-4 0 9994
2 58 28.3294 342.1942 0164980 197.5731 161.9053 13.46349118 76119
| Epoch (UTC): | 30 March 2023 01:08:28 |
| Eccentricity: | 0.0164980 |
| inclination: | 28.3294° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 342.1942° |
| argument of perigee: | 197.5731° |
| revolutions per day: | 13.46349118 |
| mean anomaly at epoch: | 161.9053° |
| orbit number at epoch: | 7611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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