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 26088.20318345 +.00000000 +00000-0 +93914-4 0 00007
2 19770 74.0430 254.9340 0005609 260.9053 271.6876 14.40316846 00
| Epoch (UTC): | 29 March 2026 04:52:35 |
| Eccentricity: | 0.0005609 |
| inclination: | 74.0430° |
| perigee height: | 753 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 254.9340° |
| argument of perigee: | 260.9053° |
| revolutions per day: | 14.40316846 |
| mean anomaly at epoch: | 271.6876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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