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 28523U 26065.22721564 +.00000000 +00000-0 +91890-4 0 00002
2 28523 82.9488 123.4826 0036069 271.9877 87.7156 13.88057039 00
| Epoch (UTC): | 06 March 2026 05:27:11 |
| Eccentricity: | 0.0036069 |
| inclination: | 82.9488° |
| perigee height: | 909 km |
| apogee height: | 962 km |
| right ascension of ascending node: | 123.4826° |
| argument of perigee: | 271.9877° |
| revolutions per day: | 13.88057039 |
| mean anomaly at epoch: | 87.7156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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