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 57985U 26145.40391764 +.00000000 +00000-0 -61726-3 0 00005
2 57985 43.0030 277.6257 0002242 267.8116 92.2479 15.27624560 04
| Epoch (UTC): | 25 May 2026 09:41:38 |
| Eccentricity: | 0.0002242 |
| inclination: | 43.0030° |
| perigee height: | 481 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.6257° |
| argument of perigee: | 267.8116° |
| revolutions per day: | 15.27624560 |
| mean anomaly at epoch: | 92.2479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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