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 40039U 26053.81744617 +.00000000 +00000-0 +19091-3 0 00006
2 40039 97.9535 356.1879 0010900 323.4885 36.5590 14.95164355 09
| Epoch (UTC): | 22 February 2026 19:37:07 |
| Eccentricity: | 0.0010900 |
| inclination: | 97.9535° |
| perigee height: | 574 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 356.1879° |
| argument of perigee: | 323.4885° |
| revolutions per day: | 14.95164355 |
| mean anomaly at epoch: | 36.5590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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