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 23026.52975409 .00002590 00000-0 13680-2 0 9997
2 00011 32.8768 75.7174 1463466 234.0024 111.6026 11.86419315388155
| Epoch (UTC): | 26 January 2023 12:42:50 |
| Eccentricity: | 0.1463466 |
| inclination: | 32.8768° |
| perigee height: | 554 km |
| apogee height: | 2930 km |
| right ascension of ascending node: | 75.7174° |
| argument of perigee: | 234.0024° |
| revolutions per day: | 11.86419315 |
| mean anomaly at epoch: | 111.6026° |
| orbit number at epoch: | 38815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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