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 51772U 26145.57342683 +.00000000 +00000-0 -13543-4 0 00002
2 51772 53.2135 353.9740 0001422 98.7826 261.3327 15.08828378 07
| Epoch (UTC): | 25 May 2026 13:45:44 |
| Eccentricity: | 0.0001422 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 353.9740° |
| argument of perigee: | 98.7826° |
| revolutions per day: | 15.08828378 |
| mean anomaly at epoch: | 261.3327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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