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 42058U 17011A 23066.76709771 0.00000000 00000-0 00000-0 0 03
2 42058 63.4415 320.7254 0062221 5.0142 354.9858 13.40859589 06
| Epoch (UTC): | 07 March 2023 18:24:37 |
| Eccentricity: | 0.0062221 |
| inclination: | 63.4415° |
| perigee height: | 1059 km |
| apogee height: | 1152 km |
| right ascension of ascending node: | 320.7254° |
| argument of perigee: | 5.0142° |
| revolutions per day: | 13.40859589 |
| mean anomaly at epoch: | 354.9858° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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