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 37187U 26064.73623781 +.00000000 +00000-0 +15787-2 0 00004
2 37187 49.5432 236.6574 5101157 136.0291 278.3428 5.40417329 09
| Epoch (UTC): | 05 March 2026 17:40:10 |
| Eccentricity: | 0.5101157 |
| inclination: | 49.5432° |
| perigee height: | 341 km |
| apogee height: | 14336 km |
| right ascension of ascending node: | 236.6574° |
| argument of perigee: | 136.0291° |
| revolutions per day: | 5.40417329 |
| mean anomaly at epoch: | 278.3428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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