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 25520U 98064B 24276.85856992 .00034338 00000-0 64315-3 0 9997
2 25520 28.4373 95.9264 0002140 161.2384 198.8295 15.47273838443001
| Epoch (UTC): | 02 October 2024 20:36:20 |
| Eccentricity: | 0.0002140 |
| inclination: | 28.4373° |
| perigee height: | 423 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 95.9264° |
| argument of perigee: | 161.2384° |
| revolutions per day: | 15.47273838 |
| mean anomaly at epoch: | 198.8295° |
| orbit number at epoch: | 44300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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