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 26067.88002028 +.00000000 +00000-0 +19805-2 0 00003
2 37187 49.5417 234.1077 5100536 138.2032 274.8106 5.40459957 07
| Epoch (UTC): | 08 March 2026 21:07:13 |
| Eccentricity: | 0.5100536 |
| inclination: | 49.5417° |
| perigee height: | 342 km |
| apogee height: | 14334 km |
| right ascension of ascending node: | 234.1077° |
| argument of perigee: | 138.2032° |
| revolutions per day: | 5.40459957 |
| mean anomaly at epoch: | 274.8106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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