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 10521U 26065.61004109 +.00000000 +00000-0 +12133-3 0 00005
2 10521 74.0262 129.2204 0018983 85.3041 275.0283 14.42391907 09
| Epoch (UTC): | 06 March 2026 14:38:27 |
| Eccentricity: | 0.0018983 |
| inclination: | 74.0262° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 129.2204° |
| argument of perigee: | 85.3041° |
| revolutions per day: | 14.42391907 |
| mean anomaly at epoch: | 275.0283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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