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 25397U 98043D 25112.43084120 .00000220 00000-0 11553-3 0 9995
2 25397 98.9676 90.5539 0001539 32.9050 327.2224 14.24299137391435
| Epoch (UTC): | 22 April 2025 10:20:24 |
| Eccentricity: | 0.0001539 |
| inclination: | 98.9676° |
| perigee height: | 810 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 90.5539° |
| argument of perigee: | 32.9050° |
| revolutions per day: | 14.24299137 |
| mean anomaly at epoch: | 327.2224° |
| orbit number at epoch: | 39143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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