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 25198.88643120 .00000897 00000-0 17721-3 0 9999
2 24797 86.8967 350.7072 0216019 180.3420 333.8390 14.47342274484223
| Epoch (UTC): | 17 July 2025 21:16:27 |
| Eccentricity: | 0.0216019 |
| inclination: | 86.8967° |
| perigee height: | 581 km |
| apogee height: | 888 km |
| right ascension of ascending node: | 350.7072° |
| argument of perigee: | 180.3420° |
| revolutions per day: | 14.47342274 |
| mean anomaly at epoch: | 333.8390° |
| orbit number at epoch: | 48422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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