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 data is extracted from the following two-line orbital elements,
1 17911U 87038A 25194.48031917 .00008612 00000-0 20936-3 0 9999
2 17911 82.5108 166.0636 0009040 87.3141 272.9140 15.40764250 88364
| Epoch (UTC): | 13 July 2025 11:31:39 |
| Eccentricity: | 0.0009040 |
| inclination: | 82.5108° |
| perigee height: | 437 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 166.0636° |
| argument of perigee: | 87.3141° |
| revolutions per day: | 15.40764250 |
| mean anomaly at epoch: | 272.9140° |
| orbit number at epoch: | 8836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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