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 23028.80211842 .00001951 00000-0 10246-2 0 9999
2 00011 32.8785 67.1784 1463529 246.8397 97.1623 11.86428138388424
| Epoch (UTC): | 28 January 2023 19:15:03 |
| Eccentricity: | 0.1463529 |
| inclination: | 32.8785° |
| perigee height: | 554 km |
| apogee height: | 2930 km |
| right ascension of ascending node: | 67.1784° |
| argument of perigee: | 246.8397° |
| revolutions per day: | 11.86428138 |
| mean anomaly at epoch: | 97.1623° |
| orbit number at epoch: | 38842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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