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 25636U 26154.14868104 +.00000000 +00000-0 +84955-4 0 00000
2 25636 96.4717 34.2255 0142226 13.5260 346.9686 14.46465039 07
| Epoch (UTC): | 03 June 2026 03:34:06 |
| Eccentricity: | 0.0142226 |
| inclination: | 96.4717° |
| perigee height: | 636 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 34.2255° |
| argument of perigee: | 13.5260° |
| revolutions per day: | 14.46465039 |
| mean anomaly at epoch: | 346.9686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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