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 58318U 26145.22833797 +.00000000 +00000-0 +49906-3 0 00008
2 58318 97.3910 235.9631 0006573 207.5969 152.4937 15.53895585 09
| Epoch (UTC): | 25 May 2026 05:28:48 |
| Eccentricity: | 0.0006573 |
| inclination: | 97.3910° |
| perigee height: | 401 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 235.9631° |
| argument of perigee: | 207.5969° |
| revolutions per day: | 15.53895585 |
| mean anomaly at epoch: | 152.4937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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