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 26087.92914051 +.00000000 +00000-0 +00000-0 0 00009
2 41836 0.0280 132.0980 0001030 233.0858 296.4070 1.00272924 05
| Epoch (UTC): | 28 March 2026 22:17:57 |
| Eccentricity: | 0.0001030 |
| inclination: | 0.0280° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 132.0980° |
| argument of perigee: | 233.0858° |
| revolutions per day: | 1.00272924 |
| mean anomaly at epoch: | 296.4070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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