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 62580U 26145.62436943 +.00000000 +00000-0 +15317-4 0 00000
2 62580 54.9790 10.0165 0012704 57.7444 302.4742 13.80605800 08
| Epoch (UTC): | 25 May 2026 14:59:05 |
| Eccentricity: | 0.0012704 |
| inclination: | 54.9790° |
| perigee height: | 952 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 10.0165° |
| argument of perigee: | 57.7444° |
| revolutions per day: | 13.80605800 |
| mean anomaly at epoch: | 302.4742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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