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 61307U 24140TU 24357.89372962 .00009287 00000-0 20330-2 0 9991
2 61307 88.8010 331.1382 0105067 285.1936 73.7673 14.54231398 16963
| Epoch (UTC): | 22 December 2024 21:26:58 |
| Eccentricity: | 0.0105067 |
| inclination: | 88.8010° |
| perigee height: | 637 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 331.1382° |
| argument of perigee: | 285.1936° |
| revolutions per day: | 14.54231398 |
| mean anomaly at epoch: | 73.7673° |
| orbit number at epoch: | 1696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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