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 37398U 26072.42359419 +.00000000 +00000-0 +29601-2 0 00007
2 37398 62.0925 89.2889 7505883 264.5577 14.6941 2.01603572 03
| Epoch (UTC): | 13 March 2026 10:09:58 |
| Eccentricity: | 0.7505883 |
| inclination: | 62.0925° |
| perigee height: | 224 km |
| apogee height: | 39958 km |
| right ascension of ascending node: | 89.2889° |
| argument of perigee: | 264.5577° |
| revolutions per day: | 2.01603572 |
| mean anomaly at epoch: | 14.6941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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