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 15772U 26072.44243043 +.00000000 +00000-0 +10268-3 0 00006
2 15772 71.1063 79.7994 0033085 121.9535 41.1642 14.21983557 05
| Epoch (UTC): | 13 March 2026 10:37:05 |
| Eccentricity: | 0.0033085 |
| inclination: | 71.1063° |
| perigee height: | 795 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 79.7994° |
| argument of perigee: | 121.9535° |
| revolutions per day: | 14.21983557 |
| mean anomaly at epoch: | 41.1642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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