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 26384U 26053.69697567 +.00000000 +00000-0 +16985-3 0 00009
2 26384 97.8305 33.2176 0013360 6.6531 353.4851 14.71149277 05
| Epoch (UTC): | 22 February 2026 16:43:38 |
| Eccentricity: | 0.0013360 |
| inclination: | 97.8305° |
| perigee height: | 648 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 33.2176° |
| argument of perigee: | 6.6531° |
| revolutions per day: | 14.71149277 |
| mean anomaly at epoch: | 353.4851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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