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 53815U 26145.62651234 +.00000000 +00000-0 +54330-3 0 00000
2 53815 97.4513 207.2655 0002249 332.9460 27.1667 15.38659843 05
| Epoch (UTC): | 25 May 2026 15:02:10 |
| Eccentricity: | 0.0002249 |
| inclination: | 97.4513° |
| perigee height: | 449 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 207.2655° |
| argument of perigee: | 332.9460° |
| revolutions per day: | 15.38659843 |
| mean anomaly at epoch: | 27.1667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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