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 41896U 26112.07339905 +.00000000 +00000-0 +12688-2 0 00006
2 41896 31.8893 30.5744 6995821 13.2301 358.2687 2.57581930 04
| Epoch (UTC): | 22 April 2026 01:45:41 |
| Eccentricity: | 0.6995821 |
| inclination: | 31.8893° |
| perigee height: | 375 km |
| apogee height: | 31828 km |
| right ascension of ascending node: | 30.5744° |
| argument of perigee: | 13.2301° |
| revolutions per day: | 2.57581930 |
| mean anomaly at epoch: | 358.2687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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