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 65184U 26145.60824549 +.00000000 +00000-0 +22453-3 0 00002
2 65184 97.4497 18.0751 0002209 76.7192 283.4282 15.05658306 01
| Epoch (UTC): | 25 May 2026 14:35:52 |
| Eccentricity: | 0.0002209 |
| inclination: | 97.4497° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0751° |
| argument of perigee: | 76.7192° |
| revolutions per day: | 15.05658306 |
| mean anomaly at epoch: | 283.4282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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