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 26033.63539458 +.00000000 +00000-0 +20296-3 0 00002
2 21809 63.2974 156.7943 0899664 72.0815 297.6150 13.55397638 03
| Epoch (UTC): | 02 February 2026 15:14:58 |
| Eccentricity: | 0.0899664 |
| inclination: | 63.2974° |
| perigee height: | 384 km |
| apogee height: | 1721 km |
| right ascension of ascending node: | 156.7943° |
| argument of perigee: | 72.0815° |
| revolutions per day: | 13.55397638 |
| mean anomaly at epoch: | 297.6150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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