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 19770U 26064.09728882 +.00000000 +00000-0 +88610-4 0 00006
2 19770 74.0446 299.4790 0005438 301.3713 209.7314 14.40305985 04
| Epoch (UTC): | 05 March 2026 02:20:05 |
| Eccentricity: | 0.0005438 |
| inclination: | 74.0446° |
| perigee height: | 754 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 299.4790° |
| argument of perigee: | 301.3713° |
| revolutions per day: | 14.40305985 |
| mean anomaly at epoch: | 209.7314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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