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 53079U 26145.23639727 +.00000000 +00000-0 +74964-4 0 00008
2 53079 97.4459 326.2983 0001460 89.1891 270.9503 15.05646254 08
| Epoch (UTC): | 25 May 2026 05:40:24 |
| Eccentricity: | 0.0001460 |
| inclination: | 97.4459° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.2983° |
| argument of perigee: | 89.1891° |
| revolutions per day: | 15.05646254 |
| mean anomaly at epoch: | 270.9503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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