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 13904U 26081.70384284 +.00000000 +00000-0 +31061-4 0 00008
2 13904 62.9509 252.7685 4785129 303.4123 19.5366 5.48372858 07
| Epoch (UTC): | 22 March 2026 16:53:32 |
| Eccentricity: | 0.4785129 |
| inclination: | 62.9509° |
| perigee height: | 706 km |
| apogee height: | 13706 km |
| right ascension of ascending node: | 252.7685° |
| argument of perigee: | 303.4123° |
| revolutions per day: | 5.48372858 |
| mean anomaly at epoch: | 19.5366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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