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 26071.27927016 +.00000000 +00000-0 +27079-3 0 00007
2 40020 97.9571 202.0936 0077993 226.5128 132.9578 14.72473185 06
| Epoch (UTC): | 12 March 2026 06:42:08 |
| Eccentricity: | 0.0077993 |
| inclination: | 97.9571° |
| perigee height: | 598 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 202.0936° |
| argument of perigee: | 226.5128° |
| revolutions per day: | 14.72473185 |
| mean anomaly at epoch: | 132.9578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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