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 26067.22073685 +.00000000 +00000-0 +12003-2 0 00003
2 37756 51.4388 9.7563 1812721 172.9134 190.1542 11.46782227 00
| Epoch (UTC): | 08 March 2026 05:17:51 |
| Eccentricity: | 0.1812721 |
| inclination: | 51.4388° |
| perigee height: | 423 km |
| apogee height: | 3434 km |
| right ascension of ascending node: | 9.7563° |
| argument of perigee: | 172.9134° |
| revolutions per day: | 11.46782227 |
| mean anomaly at epoch: | 190.1542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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