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 05732U 26088.00850177 +.00000000 +00000-0 +10488-3 0 00006
2 05732 81.2479 264.7749 0051670 25.7125 334.6595 14.06419005 05
| Epoch (UTC): | 29 March 2026 00:12:14 |
| Eccentricity: | 0.0051670 |
| inclination: | 81.2479° |
| perigee height: | 834 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 264.7749° |
| argument of perigee: | 25.7125° |
| revolutions per day: | 14.06419005 |
| mean anomaly at epoch: | 334.6595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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