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 51771U 26145.31580839 +.00000000 +00000-0 -27652-5 0 00007
2 51771 53.2142 355.1210 0001039 108.6573 251.4532 15.08834906 06
| Epoch (UTC): | 25 May 2026 07:34:45 |
| Eccentricity: | 0.0001039 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 355.1210° |
| argument of perigee: | 108.6573° |
| revolutions per day: | 15.08834906 |
| mean anomaly at epoch: | 251.4532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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