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 40107U 26152.52022397 +.00000000 +00000-0 +00000-0 0 00001
2 40107 0.0284 280.9723 0001707 150.1789 111.4460 1.00269465 05
| Epoch (UTC): | 01 June 2026 12:29:07 |
| Eccentricity: | 0.0001707 |
| inclination: | 0.0284° |
| perigee height: | 35780 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 280.9723° |
| argument of perigee: | 150.1789° |
| revolutions per day: | 1.00269465 |
| mean anomaly at epoch: | 111.4460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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