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 65592U 26145.62330163 +.00000000 +00000-0 +30004-3 0 00002
2 65592 97.4454 214.0550 0002283 157.5228 202.6099 15.05657240 07
| Epoch (UTC): | 25 May 2026 14:57:33 |
| Eccentricity: | 0.0002283 |
| inclination: | 97.4454° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.0550° |
| argument of perigee: | 157.5228° |
| revolutions per day: | 15.05657240 |
| mean anomaly at epoch: | 202.6099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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