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 40100U 26140.29003566 +.00000000 +00000-0 +00000-0 0 00002
2 40100 4.6459 76.4909 0002476 286.9013 249.0851 0.99127755 02
| Epoch (UTC): | 20 May 2026 06:57:39 |
| Eccentricity: | 0.0002476 |
| inclination: | 4.6459° |
| perigee height: | 36100 km |
| apogee height: | 36121 km |
| right ascension of ascending node: | 76.4909° |
| argument of perigee: | 286.9013° |
| revolutions per day: | 0.99127755 |
| mean anomaly at epoch: | 249.0851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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