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 05731U 26088.12176483 +.00000000 +00000-0 +84236-4 0 00002
2 05731 81.2552 98.4345 0022053 285.4431 74.4305 14.11878984 07
| Epoch (UTC): | 29 March 2026 02:55:20 |
| Eccentricity: | 0.0022053 |
| inclination: | 81.2552° |
| perigee height: | 837 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 98.4345° |
| argument of perigee: | 285.4431° |
| revolutions per day: | 14.11878984 |
| mean anomaly at epoch: | 74.4305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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