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 26129.55640998 +.00000000 +00000-0 +23292-3 0 00001
2 40908 97.4701 164.9590 0007954 47.8499 312.3427 15.50177980 06
| Epoch (UTC): | 09 May 2026 13:21:13 |
| Eccentricity: | 0.0007954 |
| inclination: | 97.4701° |
| perigee height: | 411 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 164.9590° |
| argument of perigee: | 47.8499° |
| revolutions per day: | 15.50177980 |
| mean anomaly at epoch: | 312.3427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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