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 26072.89400697 +.00000000 +00000-0 +55070-3 0 00002
2 40032 98.0734 63.9562 0009063 130.2308 229.9716 15.13757876 04
| Epoch (UTC): | 13 March 2026 21:27:22 |
| Eccentricity: | 0.0009063 |
| inclination: | 98.0734° |
| perigee height: | 518 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 63.9562° |
| argument of perigee: | 130.2308° |
| revolutions per day: | 15.13757876 |
| mean anomaly at epoch: | 229.9716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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