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 35249U 07055D 24357.78045745 .00004876 00000-0 10581-2 0 9993
2 35249 97.7752 203.7964 0215576 90.5375 272.0523 14.45018039891967
| Epoch (UTC): | 22 December 2024 18:43:51 |
| Eccentricity: | 0.0215576 |
| inclination: | 97.7752° |
| perigee height: | 588 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 203.7964° |
| argument of perigee: | 90.5375° |
| revolutions per day: | 14.45018039 |
| mean anomaly at epoch: | 272.0523° |
| orbit number at epoch: | 89196 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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