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 26067.51018091 +.00000000 +00000-0 +17506-2 0 00006
2 37187 49.5398 234.4085 5100665 137.9474 275.2346 5.40454978 05
| Epoch (UTC): | 08 March 2026 12:14:39 |
| Eccentricity: | 0.5100665 |
| inclination: | 49.5398° |
| perigee height: | 342 km |
| apogee height: | 14334 km |
| right ascension of ascending node: | 234.4085° |
| argument of perigee: | 137.9474° |
| revolutions per day: | 5.40454978 |
| mean anomaly at epoch: | 275.2346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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