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 26108.57249633 +.00000000 +00000-0 +24354-3 0 00001
2 40908 97.4734 143.2102 0008900 107.2920 252.9306 15.49465889 04
| Epoch (UTC): | 18 April 2026 13:44:23 |
| Eccentricity: | 0.0008900 |
| inclination: | 97.4734° |
| perigee height: | 412 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 143.2102° |
| argument of perigee: | 107.2920° |
| revolutions per day: | 15.49465889 |
| mean anomaly at epoch: | 252.9306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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