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 40267U 26129.93377934 +.00000000 +00000-0 +00000-0 0 00007
2 40267 0.0401 91.8465 0000964 341.4130 271.3267 1.00270962 09
| Epoch (UTC): | 09 May 2026 22:24:38 |
| Eccentricity: | 0.0000964 |
| inclination: | 0.0401° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 91.8465° |
| argument of perigee: | 341.4130° |
| revolutions per day: | 1.00270962 |
| mean anomaly at epoch: | 271.3267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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