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 26042.25249457 +.00000000 +00000-0 +76784-4 0 00006
2 21949 85.0120 146.6854 0002681 101.4504 258.6990 14.32358373 07
| Epoch (UTC): | 11 February 2026 06:03:35 |
| Eccentricity: | 0.0002681 |
| inclination: | 85.0120° |
| perigee height: | 782 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 146.6854° |
| argument of perigee: | 101.4504° |
| revolutions per day: | 14.32358373 |
| mean anomaly at epoch: | 258.6990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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