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 40761U 26072.74004166 +.00000000 +00000-0 +57167-4 0 00006
2 40761 102.4946 1.0310 0174544 157.7469 203.1267 12.11095512 03
| Epoch (UTC): | 13 March 2026 17:45:39 |
| Eccentricity: | 0.0174544 |
| inclination: | 102.4946° |
| perigee height: | 1492 km |
| apogee height: | 1771 km |
| right ascension of ascending node: | 1.0310° |
| argument of perigee: | 157.7469° |
| revolutions per day: | 12.11095512 |
| mean anomaly at epoch: | 203.1267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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