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 61348U 24140VM 24355.91556391 .00108349 00000-0 10429-1 0 9993
2 61348 88.9253 333.0927 0100268 279.3440 79.6462 14.88716165 16066
| Epoch (UTC): | 20 December 2024 21:58:24 |
| Eccentricity: | 0.0100268 |
| inclination: | 88.9253° |
| perigee height: | 532 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 333.0927° |
| argument of perigee: | 279.3440° |
| revolutions per day: | 14.88716165 |
| mean anomaly at epoch: | 79.6462° |
| orbit number at epoch: | 1606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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