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 41869U 26145.54753939 +.00000000 +00000-0 +00000-0 0 00004
2 41869 0.8101 82.9949 0041129 90.6408 83.3890 1.00272375 03
| Epoch (UTC): | 25 May 2026 13:08:27 |
| Eccentricity: | 0.0041129 |
| inclination: | 0.8101° |
| perigee height: | 35613 km |
| apogee height: | 35960 km |
| right ascension of ascending node: | 82.9949° |
| argument of perigee: | 90.6408° |
| revolutions per day: | 1.00272375 |
| mean anomaly at epoch: | 83.3890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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