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 24797U 97020F 25194.51393819 .00000748 00000-0 14730-3 0 9994
2 24797 86.8963 352.3178 0215461 195.0205 231.3086 14.47334988483628
| Epoch (UTC): | 13 July 2025 12:20:04 |
| Eccentricity: | 0.0215461 |
| inclination: | 86.8963° |
| perigee height: | 581 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 352.3178° |
| argument of perigee: | 195.0205° |
| revolutions per day: | 14.47334988 |
| mean anomaly at epoch: | 231.3086° |
| orbit number at epoch: | 48362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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