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 41121U 26144.88665426 +.00000000 +00000-0 +00000-0 0 00004
2 41121 0.0730 99.7041 0003241 319.5189 222.7060 1.00272225 07
| Epoch (UTC): | 24 May 2026 21:16:46 |
| Eccentricity: | 0.0003241 |
| inclination: | 0.0730° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 99.7041° |
| argument of perigee: | 319.5189° |
| revolutions per day: | 1.00272225 |
| mean anomaly at epoch: | 222.7060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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