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 21938U 26074.29375800 +.00000000 +00000-0 +36101-4 0 00004
2 21938 82.9328 149.6012 0027567 282.4442 141.7260 13.75549979 03
| Epoch (UTC): | 15 March 2026 07:03:00 |
| Eccentricity: | 0.0027567 |
| inclination: | 82.9328° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 149.6012° |
| argument of perigee: | 282.4442° |
| revolutions per day: | 13.75549979 |
| mean anomaly at epoch: | 141.7260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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