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 40023U 14033P 25120.25834427 .05176950 28063-5 34834-2 0 9996
2 40023 98.0543 132.6121 0014822 211.1319 148.9089 16.16570610592380
| Epoch (UTC): | 30 April 2025 06:12:00 |
| Eccentricity: | 0.0014822 |
| inclination: | 98.0543° |
| perigee height: | 219 km |
| apogee height: | 238 km |
| right ascension of ascending node: | 132.6121° |
| argument of perigee: | 211.1319° |
| revolutions per day: | 16.16570610 |
| mean anomaly at epoch: | 148.9089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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