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 25415U 26145.33851013 +.00000000 +00000-0 +32035-3 0 00008
2 25415 44.9952 352.1647 0003135 186.1640 343.5103 14.39446893 08
| Epoch (UTC): | 25 May 2026 08:07:27 |
| Eccentricity: | 0.0003135 |
| inclination: | 44.9952° |
| perigee height: | 758 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 352.1647° |
| argument of perigee: | 186.1640° |
| revolutions per day: | 14.39446893 |
| mean anomaly at epoch: | 343.5103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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