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 is defined by the following mean orbital elements,
1 25634U 26100.20113998 +.00000000 +00000-0 +53096-4 0 00002
2 25634 98.5068 68.8660 0009159 233.9127 126.1202 14.19977085 08
| Epoch (UTC): | 10 April 2026 04:49:38 |
| Eccentricity: | 0.0009159 |
| inclination: | 98.5068° |
| perigee height: | 819 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 68.8660° |
| argument of perigee: | 233.9127° |
| revolutions per day: | 14.19977085 |
| mean anomaly at epoch: | 126.1202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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