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 21949U 26135.23272442 +.00000000 +00000-0 +33288-4 0 00009
2 21949 85.0059 93.0256 0002116 110.1932 249.9488 14.32388157 02
| Epoch (UTC): | 15 May 2026 05:35:07 |
| Eccentricity: | 0.0002116 |
| inclination: | 85.0059° |
| perigee height: | 782 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 93.0256° |
| argument of perigee: | 110.1932° |
| revolutions per day: | 14.32388157 |
| mean anomaly at epoch: | 249.9488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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