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 61255C 24175N 24340.83243056 .00015535 00000+0 12803-3 0 3407
2 61255 53.1550 158.3520 0000863 90.7528 15.0716 15.69682211 14
| Epoch (UTC): | 05 December 2024 19:58:42 |
| Eccentricity: | 0.0000863 |
| inclination: | 53.1550° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 158.3520° |
| argument of perigee: | 90.7528° |
| revolutions per day: | 15.69682211 |
| mean anomaly at epoch: | 15.0716° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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