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 26072.62530005 +.00000000 +00000-0 +16088-3 0 00006
2 40069 98.5033 51.7934 0005135 325.3890 34.6953 14.21431198 06
| Epoch (UTC): | 13 March 2026 15:00:25 |
| Eccentricity: | 0.0005135 |
| inclination: | 98.5033° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 51.7934° |
| argument of perigee: | 325.3890° |
| revolutions per day: | 14.21431198 |
| mean anomaly at epoch: | 34.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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