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 40990U 26057.62012870 +.00000000 +00000-0 +00000-0 0 00001
2 40990 6.7437 80.4620 0098763 192.6237 167.2594 1.02662052 02
| Epoch (UTC): | 26 February 2026 14:52:59 |
| Eccentricity: | 0.0098763 |
| inclination: | 6.7437° |
| perigee height: | 34720 km |
| apogee height: | 35540 km |
| right ascension of ascending node: | 80.4620° |
| argument of perigee: | 192.6237° |
| revolutions per day: | 1.02662052 |
| mean anomaly at epoch: | 167.2594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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