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 26086.82177587 +.00000000 +00000-0 +56068-4 0 00004
2 21949 85.0049 120.9773 0001822 68.0453 292.0934 14.32373634 06
| Epoch (UTC): | 27 March 2026 19:43:21 |
| Eccentricity: | 0.0001822 |
| inclination: | 85.0049° |
| perigee height: | 783 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 120.9773° |
| argument of perigee: | 68.0453° |
| revolutions per day: | 14.32373634 |
| mean anomaly at epoch: | 292.0934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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