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 26039.28824301 +.00000000 +00000-0 +82359-4 0 00001
2 13618 82.9706 321.0245 0030585 291.7152 181.2923 13.77060695 08
| Epoch (UTC): | 08 February 2026 06:55:04 |
| Eccentricity: | 0.0030585 |
| inclination: | 82.9706° |
| perigee height: | 952 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 321.0245° |
| argument of perigee: | 291.7152° |
| revolutions per day: | 13.77060695 |
| mean anomaly at epoch: | 181.2923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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