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 51115U 26144.85672225 +.00000000 +00000-0 +43381-4 0 00003
2 51115 53.2168 307.1915 0001335 91.0517 269.0628 15.08842358 08
| Epoch (UTC): | 24 May 2026 20:33:40 |
| Eccentricity: | 0.0001335 |
| inclination: | 53.2168° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 307.1915° |
| argument of perigee: | 91.0517° |
| revolutions per day: | 15.08842358 |
| mean anomaly at epoch: | 269.0628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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