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 54203U 26145.34936639 +.00000000 +00000-0 +83489-4 0 00004
2 54203 53.2142 9.7857 0001160 92.5975 267.5150 15.08834683 06
| Epoch (UTC): | 25 May 2026 08:23:05 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 9.7857° |
| argument of perigee: | 92.5975° |
| revolutions per day: | 15.08834683 |
| mean anomaly at epoch: | 267.5150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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