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 26071.63981852 +.00000000 +00000-0 +89368-4 0 00008
2 40069 98.5034 50.8442 0005178 328.5531 31.5337 14.21429978 00
| Epoch (UTC): | 12 March 2026 15:21:20 |
| Eccentricity: | 0.0005178 |
| inclination: | 98.5034° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 50.8442° |
| argument of perigee: | 328.5531° |
| revolutions per day: | 14.21429978 |
| mean anomaly at epoch: | 31.5337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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