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 40908U 26037.28082541 +.00000000 +00000-0 +57165-3 0 00009
2 40908 97.4854 69.4363 0007953 21.9231 338.2357 15.46836990 05
| Epoch (UTC): | 06 February 2026 06:44:23 |
| Eccentricity: | 0.0007953 |
| inclination: | 97.4854° |
| perigee height: | 421 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 69.4363° |
| argument of perigee: | 21.9231° |
| revolutions per day: | 15.46836990 |
| mean anomaly at epoch: | 338.2357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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