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 13618U 26041.82120312 +.00000000 +00000-0 +56047-4 0 00000
2 13618 82.9704 319.1488 0030478 284.3768 138.4794 13.77060973 04
| Epoch (UTC): | 10 February 2026 19:42:31 |
| Eccentricity: | 0.0030478 |
| inclination: | 82.9704° |
| perigee height: | 952 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 319.1488° |
| argument of perigee: | 284.3768° |
| revolutions per day: | 13.77060973 |
| mean anomaly at epoch: | 138.4794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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