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 23091.93919828 .00000133 00000-0 67475-4 0 9997
2 00058 28.3293 327.5244 0164987 221.5051 137.2860 13.46349387 75962
| Epoch (UTC): | 01 April 2023 22:32:26 |
| Eccentricity: | 0.0164987 |
| inclination: | 28.3293° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 327.5244° |
| argument of perigee: | 221.5051° |
| revolutions per day: | 13.46349387 |
| mean anomaly at epoch: | 137.2860° |
| orbit number at epoch: | 7596 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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