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 28521U 26053.69514500 +.00000000 +00000-0 +62601-4 0 00006
2 28521 82.9512 130.2589 0038713 296.6423 63.0777 13.87913156 03
| Epoch (UTC): | 22 February 2026 16:41:00 |
| Eccentricity: | 0.0038713 |
| inclination: | 82.9512° |
| perigee height: | 908 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 130.2589° |
| argument of perigee: | 296.6423° |
| revolutions per day: | 13.87913156 |
| mean anomaly at epoch: | 63.0777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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