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 26077.49419641 +.00000000 +00000-0 +45328-3 0 00008
2 40024 98.0826 102.0131 0005207 127.4507 232.7205 15.28449961 03
| Epoch (UTC): | 18 March 2026 11:51:38 |
| Eccentricity: | 0.0005207 |
| inclination: | 98.0826° |
| perigee height: | 477 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 102.0131° |
| argument of perigee: | 127.4507° |
| revolutions per day: | 15.28449961 |
| mean anomaly at epoch: | 232.7205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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