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 05907U 26088.09085420 +.00000000 +00000-0 +32419-3 0 00008
2 05907 82.9671 293.6641 0021867 59.4983 55.1308 13.22468762 02
| Epoch (UTC): | 29 March 2026 02:10:49 |
| Eccentricity: | 0.0021867 |
| inclination: | 82.9671° |
| perigee height: | 1159 km |
| apogee height: | 1192 km |
| right ascension of ascending node: | 293.6641° |
| argument of perigee: | 59.4983° |
| revolutions per day: | 13.22468762 |
| mean anomaly at epoch: | 55.1308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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