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 26549U 26106.59977963 +.00000000 +00000-0 +71903-4 0 00003
2 26549 64.5483 188.2796 0038511 318.4708 41.3477 14.91018436 01
| Epoch (UTC): | 16 April 2026 14:23:40 |
| Eccentricity: | 0.0038511 |
| inclination: | 64.5483° |
| perigee height: | 568 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 188.2796° |
| argument of perigee: | 318.4708° |
| revolutions per day: | 14.91018436 |
| mean anomaly at epoch: | 41.3477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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