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 25482U 26088.01426439 +.00000000 +00000-0 +33649-3 0 00005
2 25482 45.0052 293.2919 0003949 292.2318 67.8112 14.39067619 07
| Epoch (UTC): | 29 March 2026 00:20:32 |
| Eccentricity: | 0.0003949 |
| inclination: | 45.0052° |
| perigee height: | 759 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 293.2919° |
| argument of perigee: | 292.2318° |
| revolutions per day: | 14.39067619 |
| mean anomaly at epoch: | 67.8112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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