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 55975U 26145.58383801 +.00000000 +00000-0 +28211-3 0 00005
2 55975 97.5210 318.3052 0002993 172.6197 187.5096 15.46480089 06
| Epoch (UTC): | 25 May 2026 14:00:43 |
| Eccentricity: | 0.0002993 |
| inclination: | 97.5210° |
| perigee height: | 425 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 318.3052° |
| argument of perigee: | 172.6197° |
| revolutions per day: | 15.46480089 |
| mean anomaly at epoch: | 187.5096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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