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 41241U 26144.67912373 +.00000000 +00000-0 +00000-0 0 00000
2 41241 33.1851 60.0904 0017779 181.3320 357.1274 1.00275732 09
| Epoch (UTC): | 24 May 2026 16:17:56 |
| Eccentricity: | 0.0017779 |
| inclination: | 33.1851° |
| perigee height: | 35711 km |
| apogee height: | 35860 km |
| right ascension of ascending node: | 60.0904° |
| argument of perigee: | 181.3320° |
| revolutions per day: | 1.00275732 |
| mean anomaly at epoch: | 357.1274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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