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 00188U 26105.25455851 +.00000000 +00000-0 -24856-1 0 00006
2 00188 91.1237 205.2982 0117581 93.2400 268.1933 8.93825740 09
| Epoch (UTC): | 15 April 2026 06:06:33 |
| Eccentricity: | 0.0117581 |
| inclination: | 91.1237° |
| perigee height: | 3314 km |
| apogee height: | 3545 km |
| right ascension of ascending node: | 205.2982° |
| argument of perigee: | 93.2400° |
| revolutions per day: | 8.93825740 |
| mean anomaly at epoch: | 268.1933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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