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 26072.33069983 +.00000000 +00000-0 +34424-4 0 00005
2 21938 82.9331 151.0586 0027613 288.1754 140.4512 13.75549826 08
| Epoch (UTC): | 13 March 2026 07:56:12 |
| Eccentricity: | 0.0027613 |
| inclination: | 82.9331° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 151.0586° |
| argument of perigee: | 288.1754° |
| revolutions per day: | 13.75549826 |
| mean anomaly at epoch: | 140.4512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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