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 25105U 26088.18197213 +.00000000 +00000-0 +17610-3 0 00000
2 25105 86.3908 319.4106 0010065 206.8105 153.2577 14.42462176 04
| Epoch (UTC): | 29 March 2026 04:22:02 |
| Eccentricity: | 0.0010065 |
| inclination: | 86.3908° |
| perigee height: | 743 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 319.4106° |
| argument of perigee: | 206.8105° |
| revolutions per day: | 14.42462176 |
| mean anomaly at epoch: | 153.2577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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