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 23083.19016402 .00000164 00000-0 11838-3 0 9997
2 58 28.3290 11.9095 0164999 149.0810 211.9567 13.46348945 75320
| Epoch (UTC): | 24 March 2023 04:33:50 |
| Eccentricity: | 0.0164999 |
| inclination: | 28.3290° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 11.9095° |
| argument of perigee: | 149.0810° |
| revolutions per day: | 13.46348945 |
| mean anomaly at epoch: | 211.9567° |
| orbit number at epoch: | 7532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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