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 41852U 26145.11291339 +.00000000 +00000-0 +28766-3 0 00002
2 41852 98.0717 13.5316 0002855 188.6640 171.4547 15.24020783 07
| Epoch (UTC): | 25 May 2026 02:42:35 |
| Eccentricity: | 0.0002855 |
| inclination: | 98.0717° |
| perigee height: | 492 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 13.5316° |
| argument of perigee: | 188.6640° |
| revolutions per day: | 15.24020783 |
| mean anomaly at epoch: | 171.4547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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