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 40699U 26145.60409627 +.00000000 +00000-0 +74362-4 0 00009
2 40699 98.0481 187.2830 0006230 217.4851 142.5913 14.54377573 09
| Epoch (UTC): | 25 May 2026 14:29:53 |
| Eccentricity: | 0.0006230 |
| inclination: | 98.0481° |
| perigee height: | 707 km |
| apogee height: | 716 km |
| right ascension of ascending node: | 187.2830° |
| argument of perigee: | 217.4851° |
| revolutions per day: | 14.54377573 |
| mean anomaly at epoch: | 142.5913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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