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 41836U 26032.51711727 +.00000000 +00000-0 +00000-0 0 00009
2 41836 0.0217 183.1011 0001097 136.6024 138.9043 1.00272609 03
| Epoch (UTC): | 01 February 2026 12:24:38 |
| Eccentricity: | 0.0001097 |
| inclination: | 0.0217° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 183.1011° |
| argument of perigee: | 136.6024° |
| revolutions per day: | 1.00272609 |
| mean anomaly at epoch: | 138.9043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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