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 26118.30145551 +.00000000 +00000-0 +17444-3 0 00004
2 40020 97.9661 248.1730 0080025 76.9578 284.0548 14.72602334 01
| Epoch (UTC): | 28 April 2026 07:14:05 |
| Eccentricity: | 0.0080025 |
| inclination: | 97.9661° |
| perigee height: | 597 km |
| apogee height: | 709 km |
| right ascension of ascending node: | 248.1730° |
| argument of perigee: | 76.9578° |
| revolutions per day: | 14.72602334 |
| mean anomaly at epoch: | 284.0548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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