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 40061U 26162.25166513 +.00000000 +00000-0 -41889-5 0 00006
2 40061 82.5105 311.2694 0030415 160.4848 199.7403 12.42985547 04
| Epoch (UTC): | 11 June 2026 06:02:23 |
| Eccentricity: | 0.0030415 |
| inclination: | 82.5105° |
| perigee height: | 1470 km |
| apogee height: | 1518 km |
| right ascension of ascending node: | 311.2694° |
| argument of perigee: | 160.4848° |
| revolutions per day: | 12.42985547 |
| mean anomaly at epoch: | 199.7403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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