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 21610U 26064.72621310 +.00000000 +00000-0 +14103-3 0 00005
2 21610 98.2020 117.1112 0004353 89.9282 270.2407 14.42890414 09
| Epoch (UTC): | 05 March 2026 17:25:44 |
| Eccentricity: | 0.0004353 |
| inclination: | 98.2020° |
| perigee height: | 746 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 117.1112° |
| argument of perigee: | 89.9282° |
| revolutions per day: | 14.42890414 |
| mean anomaly at epoch: | 270.2407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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