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 10025U 26017.69128271 +.00000000 +00000-0 +35364-3 0 00007
2 10025 21.7235 309.3375 7183165 38.9195 63.7653 2.22876708 08
| Epoch (UTC): | 17 January 2026 16:35:26 |
| Eccentricity: | 0.7183165 |
| inclination: | 21.7235° |
| perigee height: | 595 km |
| apogee height: | 36162 km |
| right ascension of ascending node: | 309.3375° |
| argument of perigee: | 38.9195° |
| revolutions per day: | 2.22876708 |
| mean anomaly at epoch: | 63.7653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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