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 54878U 26142.22964284 +.00000000 +00000-0 +00000-0 0 00007
2 54878 64.0309 323.6209 6942038 267.9971 18.1119 2.00663671 06
| Epoch (UTC): | 22 May 2026 05:30:41 |
| Eccentricity: | 0.6942038 |
| inclination: | 64.0309° |
| perigee height: | 1741 km |
| apogee height: | 38606 km |
| right ascension of ascending node: | 323.6209° |
| argument of perigee: | 267.9971° |
| revolutions per day: | 2.00663671 |
| mean anomaly at epoch: | 18.1119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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