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 26073.33930955 +.00000000 +00000-0 +70552-4 0 00005
2 19770 74.0433 282.4018 0005569 285.8764 246.7650 14.40310515 01
| Epoch (UTC): | 14 March 2026 08:08:36 |
| Eccentricity: | 0.0005569 |
| inclination: | 74.0433° |
| perigee height: | 753 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 282.4018° |
| argument of perigee: | 285.8764° |
| revolutions per day: | 14.40310515 |
| mean anomaly at epoch: | 246.7650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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