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 21808U 26086.81301955 +.00000000 +00000-0 +59395-3 0 00000
2 21808 63.3019 11.2106 0886303 72.9798 296.6338 13.58798480 04
| Epoch (UTC): | 27 March 2026 19:30:44 |
| Eccentricity: | 0.0886303 |
| inclination: | 63.3019° |
| perigee height: | 383 km |
| apogee height: | 1698 km |
| right ascension of ascending node: | 11.2106° |
| argument of perigee: | 72.9798° |
| revolutions per day: | 13.58798480 |
| mean anomaly at epoch: | 296.6338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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