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 40137U 26145.56632227 +.00000000 +00000-0 +15808-4 0 00005
2 40137 98.7059 147.3837 0021186 239.4146 120.4946 14.30404504 06
| Epoch (UTC): | 25 May 2026 13:35:30 |
| Eccentricity: | 0.0021186 |
| inclination: | 98.7059° |
| perigee height: | 775 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 147.3837° |
| argument of perigee: | 239.4146° |
| revolutions per day: | 14.30404504 |
| mean anomaly at epoch: | 120.4946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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