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 26135.29866519 +.00000000 +00000-0 +22527-3 0 00006
2 21808 63.2991 241.2109 0884847 73.8862 295.7666 13.59416353 04
| Epoch (UTC): | 15 May 2026 07:10:04 |
| Eccentricity: | 0.0884847 |
| inclination: | 63.2991° |
| perigee height: | 382 km |
| apogee height: | 1694 km |
| right ascension of ascending node: | 241.2109° |
| argument of perigee: | 73.8862° |
| revolutions per day: | 13.59416353 |
| mean anomaly at epoch: | 295.7666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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