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 23037.88557742 .00000120 00000-0 52121-4 0 9992
2 00058 28.3255 241.7649 0164881 133.9904 227.4362 13.46344409 68671
| Epoch (UTC): | 06 February 2023 21:15:13 |
| Eccentricity: | 0.0164881 |
| inclination: | 28.3255° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 241.7649° |
| argument of perigee: | 133.9904° |
| revolutions per day: | 13.46344409 |
| mean anomaly at epoch: | 227.4362° |
| orbit number at epoch: | 6867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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