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 21937U 26088.23781853 +.00000000 +00000-0 +33247-4 0 00009
2 21937 82.9362 174.3461 0033519 17.8443 0.1055 13.73381831 07
| Epoch (UTC): | 29 March 2026 05:42:27 |
| Eccentricity: | 0.0033519 |
| inclination: | 82.9362° |
| perigee height: | 963 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 174.3461° |
| argument of perigee: | 17.8443° |
| revolutions per day: | 13.73381831 |
| mean anomaly at epoch: | 0.1055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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