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 26070.06336891 +.00000000 +00000-0 +74405-4 0 00002
2 19770 74.0437 288.4552 0005544 291.2397 182.1337 14.40309067 05
| Epoch (UTC): | 11 March 2026 01:31:15 |
| Eccentricity: | 0.0005544 |
| inclination: | 74.0437° |
| perigee height: | 754 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 288.4552° |
| argument of perigee: | 291.2397° |
| revolutions per day: | 14.40309067 |
| mean anomaly at epoch: | 182.1337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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