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 55804U 26145.64336061 +.00000000 +00000-0 +55680-3 0 00009
2 55804 87.8934 294.2408 0002031 77.2475 282.8881 13.14501300 05
| Epoch (UTC): | 25 May 2026 15:26:26 |
| Eccentricity: | 0.0002031 |
| inclination: | 87.8934° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2408° |
| argument of perigee: | 77.2475° |
| revolutions per day: | 13.14501300 |
| mean anomaly at epoch: | 282.8881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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