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 40024U 26135.06627804 +.00000000 +00000-0 +37378-3 0 00004
2 40024 98.0745 164.5456 0001803 313.2683 46.8405 15.30355370 03
| Epoch (UTC): | 15 May 2026 01:35:26 |
| Eccentricity: | 0.0001803 |
| inclination: | 98.0745° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 164.5456° |
| argument of perigee: | 313.2683° |
| revolutions per day: | 15.30355370 |
| mean anomaly at epoch: | 46.8405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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