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 40420U 26088.15992461 +.00000000 +00000-0 +16305-3 0 00002
2 40420 97.8400 143.5237 0016769 158.7282 201.4645 15.06350411 05
| Epoch (UTC): | 29 March 2026 03:50:17 |
| Eccentricity: | 0.0016769 |
| inclination: | 97.8400° |
| perigee height: | 536 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 143.5237° |
| argument of perigee: | 158.7282° |
| revolutions per day: | 15.06350411 |
| mean anomaly at epoch: | 201.4645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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