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 26044.69753094 +.00000000 +00000-0 +65566-4 0 00009
2 21949 85.0119 145.2759 0002731 98.8758 261.2744 14.32359194 09
| Epoch (UTC): | 13 February 2026 16:44:26 |
| Eccentricity: | 0.0002731 |
| inclination: | 85.0119° |
| perigee height: | 782 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 145.2759° |
| argument of perigee: | 98.8758° |
| revolutions per day: | 14.32359194 |
| mean anomaly at epoch: | 261.2744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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