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 21666U 26104.11383609 +.00000000 +00000-0 +46514-4 0 00002
2 21666 82.9075 156.9770 0025764 33.7977 355.1945 13.73534370 07
| Epoch (UTC): | 14 April 2026 02:43:55 |
| Eccentricity: | 0.0025764 |
| inclination: | 82.9075° |
| perigee height: | 968 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 156.9770° |
| argument of perigee: | 33.7977° |
| revolutions per day: | 13.73534370 |
| mean anomaly at epoch: | 355.1945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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