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 41604U 26022.73596191 +.00000000 +00000-0 +11778-3 0 00008
2 41604 97.0481 61.6306 0009019 275.2378 84.7900 16.52384104 03
| Epoch (UTC): | 22 January 2026 17:39:47 |
| Eccentricity: | 0.0009019 |
| inclination: | 97.0481° |
| perigee height: | 127 km |
| apogee height: | 139 km |
| right ascension of ascending node: | 61.6306° |
| argument of perigee: | 275.2378° |
| revolutions per day: | 16.52384104 |
| mean anomaly at epoch: | 84.7900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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