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 40032U 26110.43156419 +.00000000 +00000-0 +27490-3 0 00000
2 40032 98.0758 103.7557 0008150 26.1490 334.0150 15.14386934 02
| Epoch (UTC): | 20 April 2026 10:21:27 |
| Eccentricity: | 0.0008150 |
| inclination: | 98.0758° |
| perigee height: | 517 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 103.7557° |
| argument of perigee: | 26.1490° |
| revolutions per day: | 15.14386934 |
| mean anomaly at epoch: | 334.0150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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