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 07434U 74071B 24357.86687461 .00000439 00000-0 15416-3 0 9990
2 07434 74.0442 209.5600 0020238 164.6756 195.5015 14.37793987630769
| Epoch (UTC): | 22 December 2024 20:48:17 |
| Eccentricity: | 0.0020238 |
| inclination: | 74.0442° |
| perigee height: | 751 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 209.5600° |
| argument of perigee: | 164.6756° |
| revolutions per day: | 14.37793987 |
| mean anomaly at epoch: | 195.5015° |
| orbit number at epoch: | 63076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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