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 40061U 26145.59003707 +.00000000 +00000-0 -48086-4 0 00004
2 40061 82.5102 321.6227 0029636 196.6811 163.3296 12.42984483 07
| Epoch (UTC): | 25 May 2026 14:09:39 |
| Eccentricity: | 0.0029636 |
| inclination: | 82.5102° |
| perigee height: | 1471 km |
| apogee height: | 1517 km |
| right ascension of ascending node: | 321.6227° |
| argument of perigee: | 196.6811° |
| revolutions per day: | 12.42984483 |
| mean anomaly at epoch: | 163.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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