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 25417U 26100.17246259 +.00000000 +00000-0 +37480-3 0 00002
2 25417 44.9929 201.3831 0003391 328.8161 31.2486 14.39929415 02
| Epoch (UTC): | 10 April 2026 04:08:20 |
| Eccentricity: | 0.0003391 |
| inclination: | 44.9929° |
| perigee height: | 756 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 201.3831° |
| argument of perigee: | 328.8161° |
| revolutions per day: | 14.39929415 |
| mean anomaly at epoch: | 31.2486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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