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 40042U 26073.31879152 +.00000000 +00000-0 +87316-3 0 00005
2 40042 98.1051 90.8193 0009529 115.2282 244.9945 15.29777767 07
| Epoch (UTC): | 14 March 2026 07:39:03 |
| Eccentricity: | 0.0009529 |
| inclination: | 98.1051° |
| perigee height: | 470 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 90.8193° |
| argument of perigee: | 115.2282° |
| revolutions per day: | 15.29777767 |
| mean anomaly at epoch: | 244.9945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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