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 26106.52472662 +.00000000 +00000-0 +75068-4 0 00002
2 18362 90.3682 84.3331 0103383 250.2180 232.4050 13.44470290 08
| Epoch (UTC): | 16 April 2026 12:35:36 |
| Eccentricity: | 0.0103383 |
| inclination: | 90.3682° |
| perigee height: | 1015 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 84.3331° |
| argument of perigee: | 250.2180° |
| revolutions per day: | 13.44470290 |
| mean anomaly at epoch: | 232.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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