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 25400U 98043G 25339.29076437 .00000168 00000-0 89248-4 0 9995
2 25400 98.8113 287.0675 0008892 290.8627 69.1600 14.26022792425535
| Epoch (UTC): | 05 December 2025 06:58:42 |
| Eccentricity: | 0.0008892 |
| inclination: | 98.8113° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 287.0675° |
| argument of perigee: | 290.8627° |
| revolutions per day: | 14.26022792 |
| mean anomaly at epoch: | 69.1600° |
| orbit number at epoch: | 42553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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