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 26088.13550066 +.00000000 +00000-0 +59628-4 0 00008
2 62580 54.9770 211.0693 0008570 302.7167 57.2962 13.80545337 03
| Epoch (UTC): | 29 March 2026 03:15:07 |
| Eccentricity: | 0.0008570 |
| inclination: | 54.9770° |
| perigee height: | 956 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 211.0693° |
| argument of perigee: | 302.7167° |
| revolutions per day: | 13.80545337 |
| mean anomaly at epoch: | 57.2962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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