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 21809U 26069.93140958 +.00000000 +00000-0 +36819-3 0 00005
2 21809 63.2972 60.0277 0900063 72.7815 296.9640 13.55653715 08
| Epoch (UTC): | 10 March 2026 22:21:13 |
| Eccentricity: | 0.0900063 |
| inclination: | 63.2972° |
| perigee height: | 383 km |
| apogee height: | 1720 km |
| right ascension of ascending node: | 60.0277° |
| argument of perigee: | 72.7815° |
| revolutions per day: | 13.55653715 |
| mean anomaly at epoch: | 296.9640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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