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 55996U 26145.59253338 +.00000000 +00000-0 +72296-3 0 00002
2 55996 43.0049 345.0556 0001020 266.0082 94.0653 15.26889610 04
| Epoch (UTC): | 25 May 2026 14:13:14 |
| Eccentricity: | 0.0001020 |
| inclination: | 43.0049° |
| perigee height: | 484 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 345.0556° |
| argument of perigee: | 266.0082° |
| revolutions per day: | 15.26889610 |
| mean anomaly at epoch: | 94.0653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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