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 65292U 26145.57640841 +.00000000 +00000-0 +17324-3 0 00000
2 65292 97.4503 198.1273 0002399 100.7948 259.3549 15.05655517 04
| Epoch (UTC): | 25 May 2026 13:50:01 |
| Eccentricity: | 0.0002399 |
| inclination: | 97.4503° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 198.1273° |
| argument of perigee: | 100.7948° |
| revolutions per day: | 15.05655517 |
| mean anomaly at epoch: | 259.3549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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