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 26033.59082601 +.00000000 +00000-0 +28520-3 0 00007
2 21808 63.3001 153.7409 0886952 71.9755 297.5819 13.58167793 06
| Epoch (UTC): | 02 February 2026 14:10:47 |
| Eccentricity: | 0.0886952 |
| inclination: | 63.3001° |
| perigee height: | 384 km |
| apogee height: | 1701 km |
| right ascension of ascending node: | 153.7409° |
| argument of perigee: | 71.9755° |
| revolutions per day: | 13.58167793 |
| mean anomaly at epoch: | 297.5819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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