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 37218U 26145.47193443 +.00000000 +00000-0 +00000-0 0 00007
2 37218 5.0792 50.8806 0003108 14.4297 246.3479 1.00272804 01
| Epoch (UTC): | 25 May 2026 11:19:35 |
| Eccentricity: | 0.0003108 |
| inclination: | 5.0792° |
| perigee height: | 35773 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 50.8806° |
| argument of perigee: | 14.4297° |
| revolutions per day: | 1.00272804 |
| mean anomaly at epoch: | 246.3479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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