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 26104.00607264 +.00000000 +00000-0 +25392-3 0 00005
2 21809 63.2985 329.1367 0899651 73.4355 296.3462 13.56037899 04
| Epoch (UTC): | 14 April 2026 00:08:44 |
| Eccentricity: | 0.0899651 |
| inclination: | 63.2985° |
| perigee height: | 382 km |
| apogee height: | 1718 km |
| right ascension of ascending node: | 329.1367° |
| argument of perigee: | 73.4355° |
| revolutions per day: | 13.56037899 |
| mean anomaly at epoch: | 296.3462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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