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 26072U 00007B 24357.80643216 .00066408 00000-0 20856-2 0 9992
2 26072 18.0696 208.2851 3383830 159.0421 219.0656 8.65432450307922
| Epoch (UTC): | 22 December 2024 19:21:15 |
| Eccentricity: | 0.3383830 |
| inclination: | 18.0696° |
| perigee height: | 252 km |
| apogee height: | 7034 km |
| right ascension of ascending node: | 208.2851° |
| argument of perigee: | 159.0421° |
| revolutions per day: | 8.65432450 |
| mean anomaly at epoch: | 219.0656° |
| orbit number at epoch: | 30792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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