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 39975U 26084.68641682 +.00000000 +00000-0 +46438-3 0 00005
2 39975 82.5954 227.3826 0095885 334.8358 24.8157 14.04820984 04
| Epoch (UTC): | 25 March 2026 16:28:26 |
| Eccentricity: | 0.0095885 |
| inclination: | 82.5954° |
| perigee height: | 808 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 227.3826° |
| argument of perigee: | 334.8358° |
| revolutions per day: | 14.04820984 |
| mean anomaly at epoch: | 24.8157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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