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 41188U 26145.10405992 +.00000000 +00000-0 +13868-3 0 00002
2 41188 47.0017 289.9716 0002409 109.6740 250.4406 14.58830341 05
| Epoch (UTC): | 25 May 2026 02:29:50 |
| Eccentricity: | 0.0002409 |
| inclination: | 47.0017° |
| perigee height: | 695 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 289.9716° |
| argument of perigee: | 109.6740° |
| revolutions per day: | 14.58830341 |
| mean anomaly at epoch: | 250.4406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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