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 40071U 26073.59510066 +.00000000 +00000-0 +60773-4 0 00002
2 40071 98.3759 29.6395 0006119 212.6110 147.4728 14.89645253 09
| Epoch (UTC): | 14 March 2026 14:16:56 |
| Eccentricity: | 0.0006119 |
| inclination: | 98.3759° |
| perigee height: | 595 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 29.6395° |
| argument of perigee: | 212.6110° |
| revolutions per day: | 14.89645253 |
| mean anomaly at epoch: | 147.4728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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