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 25196.94327032 .00000791 00000-0 15595-3 0 9995
2 24797 86.8965 351.4229 0215769 186.8622 289.1400 14.47338572483948
| Epoch (UTC): | 15 July 2025 22:38:18 |
| Eccentricity: | 0.0215769 |
| inclination: | 86.8965° |
| perigee height: | 581 km |
| apogee height: | 888 km |
| right ascension of ascending node: | 351.4229° |
| argument of perigee: | 186.8622° |
| revolutions per day: | 14.47338572 |
| mean anomaly at epoch: | 289.1400° |
| orbit number at epoch: | 48394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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