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 40977U 26145.28002549 +.00000000 +00000-0 +35911-3 0 00000
2 40977 64.7739 347.3421 0118426 67.2902 294.0679 14.93820160 08
| Epoch (UTC): | 25 May 2026 06:43:14 |
| Eccentricity: | 0.0118426 |
| inclination: | 64.7739° |
| perigee height: | 504 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 347.3421° |
| argument of perigee: | 67.2902° |
| revolutions per day: | 14.93820160 |
| mean anomaly at epoch: | 294.0679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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