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 65179U 26145.61931942 +.00000000 +00000-0 +19596-3 0 00007
2 65179 97.4476 18.0592 0001739 85.9401 274.2025 15.05658033 07
| Epoch (UTC): | 25 May 2026 14:51:49 |
| Eccentricity: | 0.0001739 |
| inclination: | 97.4476° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0592° |
| argument of perigee: | 85.9401° |
| revolutions per day: | 15.05658033 |
| mean anomaly at epoch: | 274.2025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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