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 41919U 26145.41437811 +.00000000 +00000-0 +14959-4 0 00006
2 41919 86.3952 98.0350 0002351 85.9284 274.2181 14.34217967 00
| Epoch (UTC): | 25 May 2026 09:56:42 |
| Eccentricity: | 0.0002351 |
| inclination: | 86.3952° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 98.0350° |
| argument of perigee: | 85.9284° |
| revolutions per day: | 14.34217967 |
| mean anomaly at epoch: | 274.2181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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