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 23027.80139130 .00000130 00000-0 72537-4 0 9994
2 00058 28.3274 292.9285 0164854 50.5096 310.9903 13.46343599 67310
| Epoch (UTC): | 27 January 2023 19:14:00 |
| Eccentricity: | 0.0164854 |
| inclination: | 28.3274° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 292.9285° |
| argument of perigee: | 50.5096° |
| revolutions per day: | 13.46343599 |
| mean anomaly at epoch: | 310.9903° |
| orbit number at epoch: | 6731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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