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 39984U 26084.96045676 +.00000000 +00000-0 +13092-2 0 00006
2 39984 82.8298 343.0506 0011314 5.2228 354.9078 14.35408140 08
| Epoch (UTC): | 25 March 2026 23:03:03 |
| Eccentricity: | 0.0011314 |
| inclination: | 82.8298° |
| perigee height: | 766 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 343.0506° |
| argument of perigee: | 5.2228° |
| revolutions per day: | 14.35408140 |
| mean anomaly at epoch: | 354.9078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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