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 08366U 26053.64844825 +.00000000 +00000-0 +00000-0 0 00003
2 08366 4.8989 278.8680 0005611 358.5758 349.1229 1.00235530 05
| Epoch (UTC): | 22 February 2026 15:33:45 |
| Eccentricity: | 0.0005611 |
| inclination: | 4.8989° |
| perigee height: | 35773 km |
| apogee height: | 35820 km |
| right ascension of ascending node: | 278.8680° |
| argument of perigee: | 358.5758° |
| revolutions per day: | 1.00235530 |
| mean anomaly at epoch: | 349.1229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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