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 41019U 26144.84405742 +.00000000 +00000-0 +00000-0 0 00009
2 41019 56.9441 31.7103 0111404 231.2784 127.7540 2.00567019 05
| Epoch (UTC): | 24 May 2026 20:15:26 |
| Eccentricity: | 0.0111404 |
| inclination: | 56.9441° |
| perigee height: | 19886 km |
| apogee height: | 20478 km |
| right ascension of ascending node: | 31.7103° |
| argument of perigee: | 231.2784° |
| revolutions per day: | 2.00567019 |
| mean anomaly at epoch: | 127.7540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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