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 25634U 99008A 25342.94529043 .00000153 00000-0 91440-4 0 9999
2 25634 98.4868 311.4797 0009266 227.8507 132.1884 14.19941103387302
| Epoch (UTC): | 08 December 2025 22:41:13 |
| Eccentricity: | 0.0009266 |
| inclination: | 98.4868° |
| perigee height: | 819 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 311.4797° |
| argument of perigee: | 227.8507° |
| revolutions per day: | 14.19941103 |
| mean anomaly at epoch: | 132.1884° |
| orbit number at epoch: | 38730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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