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 40047U 26032.28146785 +.00000000 +00000-0 +61276-4 0 00008
2 40047 97.8897 276.1968 0566635 296.1168 58.2736 13.61942687 06
| Epoch (UTC): | 01 February 2026 06:45:18 |
| Eccentricity: | 0.0566635 |
| inclination: | 97.8897° |
| perigee height: | 609 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 276.1968° |
| argument of perigee: | 296.1168° |
| revolutions per day: | 13.61942687 |
| mean anomaly at epoch: | 58.2736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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