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 51875U 26145.09591716 +.00000000 +00000-0 +44313-4 0 00004
2 51875 53.2128 26.0301 0001358 75.3499 284.7644 15.08836557 08
| Epoch (UTC): | 25 May 2026 02:18:07 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.0301° |
| argument of perigee: | 75.3499° |
| revolutions per day: | 15.08836557 |
| mean anomaly at epoch: | 284.7644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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