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 40075U 26087.83494201 +.00000000 +00000-0 +29724-3 0 00000
2 40075 98.3963 55.4048 0005148 148.9626 211.1897 14.93181720 01
| Epoch (UTC): | 28 March 2026 20:02:18 |
| Eccentricity: | 0.0005148 |
| inclination: | 98.3963° |
| perigee height: | 584 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 55.4048° |
| argument of perigee: | 148.9626° |
| revolutions per day: | 14.93181720 |
| mean anomaly at epoch: | 211.1897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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