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 26065.09158678 +.00000000 +00000-0 +30677-2 0 00009
2 41896 31.7668 49.2549 6997996 344.5062 1.8111 2.57457617 09
| Epoch (UTC): | 06 March 2026 02:11:53 |
| Eccentricity: | 0.6997996 |
| inclination: | 31.7668° |
| perigee height: | 372 km |
| apogee height: | 31845 km |
| right ascension of ascending node: | 49.2549° |
| argument of perigee: | 344.5062° |
| revolutions per day: | 2.57457617 |
| mean anomaly at epoch: | 1.8111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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