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 41923U 26145.61099839 +.00000000 +00000-0 +13006-4 0 00009
2 41923 86.3950 97.9022 0002464 86.4405 273.7072 14.34218002 07
| Epoch (UTC): | 25 May 2026 14:39:50 |
| Eccentricity: | 0.0002464 |
| inclination: | 86.3950° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.9022° |
| argument of perigee: | 86.4405° |
| revolutions per day: | 14.34218002 |
| mean anomaly at epoch: | 273.7072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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