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 18362U 26104.19432764 +.00000000 +00000-0 +89287-4 0 00000
2 18362 90.3678 84.2473 0103342 257.0158 112.9314 13.44469953 03
| Epoch (UTC): | 14 April 2026 04:39:49 |
| Eccentricity: | 0.0103342 |
| inclination: | 90.3678° |
| perigee height: | 1015 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 84.2473° |
| argument of perigee: | 257.0158° |
| revolutions per day: | 13.44469953 |
| mean anomaly at epoch: | 112.9314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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