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 53833U 26145.20037197 +.00000000 +00000-0 +38004-5 0 00002
2 53833 53.2141 320.5268 0001316 84.9699 275.1443 15.08848024 08
| Epoch (UTC): | 25 May 2026 04:48:32 |
| Eccentricity: | 0.0001316 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 320.5268° |
| argument of perigee: | 84.9699° |
| revolutions per day: | 15.08848024 |
| mean anomaly at epoch: | 275.1443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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