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 55383U 26145.58852189 +.00000000 +00000-0 +33170-4 0 00009
2 55383 43.0041 214.4351 0002361 286.6373 73.4219 15.27575639 01
| Epoch (UTC): | 25 May 2026 14:07:28 |
| Eccentricity: | 0.0002361 |
| inclination: | 43.0041° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 214.4351° |
| argument of perigee: | 286.6373° |
| revolutions per day: | 15.27575639 |
| mean anomaly at epoch: | 73.4219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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