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 56926U 26145.61960360 +.00000000 +00000-0 -16656-4 0 00009
2 56926 43.0047 356.2111 0001480 253.3184 106.7505 15.27576913 06
| Epoch (UTC): | 25 May 2026 14:52:13 |
| Eccentricity: | 0.0001480 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.2111° |
| argument of perigee: | 253.3184° |
| revolutions per day: | 15.27576913 |
| mean anomaly at epoch: | 106.7505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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