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 32954U 26104.22903855 +.00000000 +00000-0 -37458-4 0 00005
2 32954 82.5042 37.2203 0021510 107.1198 47.4577 12.42757783 09
| Epoch (UTC): | 14 April 2026 05:29:48 |
| Eccentricity: | 0.0021510 |
| inclination: | 82.5042° |
| perigee height: | 1478 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 37.2203° |
| argument of perigee: | 107.1198° |
| revolutions per day: | 12.42757783 |
| mean anomaly at epoch: | 47.4577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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