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 40046U 26156.41506041 +.00000000 +00000-0 +60593-3 0 00004
2 40046 97.7222 323.2534 0039123 48.9903 311.4692 14.99431467 02
| Epoch (UTC): | 05 June 2026 09:57:41 |
| Eccentricity: | 0.0039123 |
| inclination: | 97.7222° |
| perigee height: | 541 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 323.2534° |
| argument of perigee: | 48.9903° |
| revolutions per day: | 14.99431467 |
| mean anomaly at epoch: | 311.4692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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