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 40076U 26077.39503414 +.00000000 +00000-0 +36664-3 0 00009
2 40076 98.3780 60.7407 0005510 199.0516 161.0507 15.11750424 00
| Epoch (UTC): | 18 March 2026 09:28:50 |
| Eccentricity: | 0.0005510 |
| inclination: | 98.3780° |
| perigee height: | 527 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 60.7407° |
| argument of perigee: | 199.0516° |
| revolutions per day: | 15.11750424 |
| mean anomaly at epoch: | 161.0507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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