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 26145.61161280 +.00000000 +00000-0 +00000-0 0 00008
2 41836 0.0083 152.3218 0001145 316.3360 135.4892 1.00270215 00
| Epoch (UTC): | 25 May 2026 14:40:43 |
| Eccentricity: | 0.0001145 |
| inclination: | 0.0083° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 152.3218° |
| argument of perigee: | 316.3360° |
| revolutions per day: | 1.00270215 |
| mean anomaly at epoch: | 135.4892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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