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 40072U 26156.42461044 +.00000000 +00000-0 +17931-3 0 00005
2 40072 98.3832 114.7197 0004756 329.7638 30.3302 14.87996518 07
| Epoch (UTC): | 05 June 2026 10:11:26 |
| Eccentricity: | 0.0004756 |
| inclination: | 98.3832° |
| perigee height: | 601 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 114.7197° |
| argument of perigee: | 329.7638° |
| revolutions per day: | 14.87996518 |
| mean anomaly at epoch: | 30.3302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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