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 26086.74879705 +.00000000 +00000-0 +42326-3 0 00002
2 21809 63.2994 15.1755 0899936 73.1065 296.6580 13.55818822 04
| Epoch (UTC): | 27 March 2026 17:58:16 |
| Eccentricity: | 0.0899936 |
| inclination: | 63.2994° |
| perigee height: | 382 km |
| apogee height: | 1719 km |
| right ascension of ascending node: | 15.1755° |
| argument of perigee: | 73.1065° |
| revolutions per day: | 13.55818822 |
| mean anomaly at epoch: | 296.6580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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