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 15453U 26140.33671756 +.00000000 +00000-0 +00000-0 0 00002
2 15453 11.5385 321.1417 0002315 306.9235 236.6898 0.98858412 08
| Epoch (UTC): | 20 May 2026 08:04:52 |
| Eccentricity: | 0.0002315 |
| inclination: | 11.5385° |
| perigee height: | 36178 km |
| apogee height: | 36197 km |
| right ascension of ascending node: | 321.1417° |
| argument of perigee: | 306.9235° |
| revolutions per day: | 0.98858412 |
| mean anomaly at epoch: | 236.6898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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