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 40049U 26087.97654867 +.00000000 +00000-0 +47831-3 0 00001
2 40049 98.0989 82.0264 0007158 147.5733 212.5935 15.09457873 01
| Epoch (UTC): | 28 March 2026 23:26:13 |
| Eccentricity: | 0.0007158 |
| inclination: | 98.0989° |
| perigee height: | 533 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 82.0264° |
| argument of perigee: | 147.5733° |
| revolutions per day: | 15.09457873 |
| mean anomaly at epoch: | 212.5935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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