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 26069.96786564 +.00000000 +00000-0 +39697-3 0 00006
2 40071 98.3764 25.8005 0005853 224.8044 135.2699 14.89635787 09
| Epoch (UTC): | 10 March 2026 23:13:43 |
| Eccentricity: | 0.0005853 |
| inclination: | 98.3764° |
| perigee height: | 595 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 25.8005° |
| argument of perigee: | 224.8044° |
| revolutions per day: | 14.89635787 |
| mean anomaly at epoch: | 135.2699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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