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 26106.19054926 +.00000000 +00000-0 +23517-4 0 00006
2 25634 98.5078 74.6252 0009391 214.8324 145.2239 14.19977882 03
| Epoch (UTC): | 16 April 2026 04:34:23 |
| Eccentricity: | 0.0009391 |
| inclination: | 98.5078° |
| perigee height: | 819 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 74.6252° |
| argument of perigee: | 214.8324° |
| revolutions per day: | 14.19977882 |
| mean anomaly at epoch: | 145.2239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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