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 37818U 26086.17022861 +.00000000 +00000-0 +99974-3 0 00000
2 37818 62.8229 175.9069 4627240 281.2487 31.8055 6.15179485 00
| Epoch (UTC): | 27 March 2026 04:05:07 |
| Eccentricity: | 0.4627240 |
| inclination: | 62.8229° |
| perigee height: | 382 km |
| apogee height: | 12025 km |
| right ascension of ascending node: | 175.9069° |
| argument of perigee: | 281.2487° |
| revolutions per day: | 6.15179485 |
| mean anomaly at epoch: | 31.8055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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