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 61101U 24140NT 24357.72702981 .00000548 00000-0 26112-3 0 9999
2 61101 89.0271 336.0769 0056388 157.4616 202.9068 14.17135165 16516
| Epoch (UTC): | 22 December 2024 17:26:55 |
| Eccentricity: | 0.0056388 |
| inclination: | 89.0271° |
| perigee height: | 794 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 336.0769° |
| argument of perigee: | 157.4616° |
| revolutions per day: | 14.17135165 |
| mean anomaly at epoch: | 202.9068° |
| orbit number at epoch: | 1651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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