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 26076.32597131 +.00000000 +00000-0 +56674-4 0 00001
2 19770 74.0429 276.8826 0005575 280.7582 251.8269 14.40311514 02
| Epoch (UTC): | 17 March 2026 07:49:23 |
| Eccentricity: | 0.0005575 |
| inclination: | 74.0429° |
| perigee height: | 753 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 276.8826° |
| argument of perigee: | 280.7582° |
| revolutions per day: | 14.40311514 |
| mean anomaly at epoch: | 251.8269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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