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 26044.91360043 +.00000000 +00000-0 +33739-3 0 00004
2 40908 97.4850 77.3256 0007066 354.9049 5.2128 15.47112042 04
| Epoch (UTC): | 13 February 2026 21:55:35 |
| Eccentricity: | 0.0007066 |
| inclination: | 97.4850° |
| perigee height: | 420 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 77.3256° |
| argument of perigee: | 354.9049° |
| revolutions per day: | 15.47112042 |
| mean anomaly at epoch: | 5.2128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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