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 26066.73832647 +.00000000 +00000-0 +96417-4 0 00007
2 21938 82.9339 155.2101 0027748 304.4836 166.4433 13.75549342 00
| Epoch (UTC): | 07 March 2026 17:43:11 |
| Eccentricity: | 0.0027748 |
| inclination: | 82.9339° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 155.2101° |
| argument of perigee: | 304.4836° |
| revolutions per day: | 13.75549342 |
| mean anomaly at epoch: | 166.4433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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