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 53913U 26145.51866671 +.00000000 +00000-0 -96896-5 0 00006
2 53913 53.2151 329.2028 0001312 89.6002 270.5140 15.08836505 08
| Epoch (UTC): | 25 May 2026 12:26:52 |
| Eccentricity: | 0.0001312 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.2028° |
| argument of perigee: | 89.6002° |
| revolutions per day: | 15.08836505 |
| mean anomaly at epoch: | 270.5140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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