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 00011U 59001A 23029.47544809 .00001868 00000-0 97986-3 0 9999
2 00011 32.8790 64.6480 1463553 250.6435 93.0546 11.86430801388506
| Epoch (UTC): | 29 January 2023 11:24:38 |
| Eccentricity: | 0.1463553 |
| inclination: | 32.8790° |
| perigee height: | 554 km |
| apogee height: | 2930 km |
| right ascension of ascending node: | 64.6480° |
| argument of perigee: | 250.6435° |
| revolutions per day: | 11.86430801 |
| mean anomaly at epoch: | 93.0546° |
| orbit number at epoch: | 38850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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