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 53870U 26145.66310141 +.00000000 +00000-0 +19410-4 0 00005
2 53870 53.2143 278.5048 0001208 81.8171 278.2958 15.08835399 06
| Epoch (UTC): | 25 May 2026 15:54:51 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 278.5048° |
| argument of perigee: | 81.8171° |
| revolutions per day: | 15.08835399 |
| mean anomaly at epoch: | 278.2958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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