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 40020U 26145.34416846 +.00000000 +00000-0 +93336-4 0 00001
2 40020 97.9709 274.6977 0078344 351.0681 8.9127 14.72640483 07
| Epoch (UTC): | 25 May 2026 08:15:36 |
| Eccentricity: | 0.0078344 |
| inclination: | 97.9709° |
| perigee height: | 598 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 274.6977° |
| argument of perigee: | 351.0681° |
| revolutions per day: | 14.72640483 |
| mean anomaly at epoch: | 8.9127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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