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 55041U 26145.62375749 +.00000000 +00000-0 +48680-3 0 00008
2 55041 97.3191 221.9956 0005460 146.1049 214.0560 15.64376591 06
| Epoch (UTC): | 25 May 2026 14:58:12 |
| Eccentricity: | 0.0005460 |
| inclination: | 97.3191° |
| perigee height: | 371 km |
| apogee height: | 379 km |
| right ascension of ascending node: | 221.9956° |
| argument of perigee: | 146.1049° |
| revolutions per day: | 15.64376591 |
| mean anomaly at epoch: | 214.0560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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