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 65176U 26145.23165169 +.00000000 +00000-0 +44370-3 0 00000
2 65176 97.4473 17.6586 0002606 82.9864 277.1660 15.05671751 02
| Epoch (UTC): | 25 May 2026 05:33:34 |
| Eccentricity: | 0.0002606 |
| inclination: | 97.4473° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.6586° |
| argument of perigee: | 82.9864° |
| revolutions per day: | 15.05671751 |
| mean anomaly at epoch: | 277.1660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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