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 24971U 97057A 25342.97991583 .00000331 00000-0 12910-3 0 9991
2 24971 98.8289 327.7744 0053153 68.3177 292.3655 14.35408326475321
| Epoch (UTC): | 08 December 2025 23:31:04 |
| Eccentricity: | 0.0053153 |
| inclination: | 98.8289° |
| perigee height: | 735 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 327.7744° |
| argument of perigee: | 68.3177° |
| revolutions per day: | 14.35408326 |
| mean anomaly at epoch: | 292.3655° |
| orbit number at epoch: | 47532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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