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 40069U 26073.61078189 +.00000000 +00000-0 +42076-4 0 00003
2 40069 98.5032 52.7426 0005103 322.4027 37.6793 14.21430958 05
| Epoch (UTC): | 14 March 2026 14:39:31 |
| Eccentricity: | 0.0005103 |
| inclination: | 98.5032° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 52.7426° |
| argument of perigee: | 322.4027° |
| revolutions per day: | 14.21430958 |
| mean anomaly at epoch: | 37.6793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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