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 37756U 26067.83072285 +.00000000 +00000-0 +10999-2 0 00007
2 37756 51.4389 8.1492 1812675 174.1281 188.4357 11.46788594 07
| Epoch (UTC): | 08 March 2026 19:56:14 |
| Eccentricity: | 0.1812675 |
| inclination: | 51.4389° |
| perigee height: | 423 km |
| apogee height: | 3434 km |
| right ascension of ascending node: | 8.1492° |
| argument of perigee: | 174.1281° |
| revolutions per day: | 11.46788594 |
| mean anomaly at epoch: | 188.4357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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