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 40367U 26144.74788888 +.00000000 +00000-0 +00000-0 0 00008
2 40367 5.5826 73.0946 0002791 140.6485 37.1308 1.00260302 00
| Epoch (UTC): | 24 May 2026 17:56:57 |
| Eccentricity: | 0.0002791 |
| inclination: | 5.5826° |
| perigee height: | 35778 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 73.0946° |
| argument of perigee: | 140.6485° |
| revolutions per day: | 1.00260302 |
| mean anomaly at epoch: | 37.1308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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