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 49401U 26145.56548174 +.00000000 +00000-0 +21454-3 0 00008
2 49401 97.3312 183.2826 0013767 316.5094 43.5055 15.20232809 01
| Epoch (UTC): | 25 May 2026 13:34:17 |
| Eccentricity: | 0.0013767 |
| inclination: | 97.3312° |
| perigee height: | 496 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 183.2826° |
| argument of perigee: | 316.5094° |
| revolutions per day: | 15.20232809 |
| mean anomaly at epoch: | 43.5055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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