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 25861U 99039B 24282.85777841 .00003110 00000-0 41222-3 0 9996
2 25861 98.0754 329.6221 0016261 128.8882 231.3783 14.80519798360351
| Epoch (UTC): | 08 October 2024 20:35:12 |
| Eccentricity: | 0.0016261 |
| inclination: | 98.0754° |
| perigee height: | 616 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 329.6221° |
| argument of perigee: | 128.8882° |
| revolutions per day: | 14.80519798 |
| mean anomaly at epoch: | 231.3783° |
| orbit number at epoch: | 36035 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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