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 59873U 26145.58050086 +.00000000 +00000-0 -28010-5 0 00002
2 59873 43.0010 196.1417 0001094 275.7094 84.3633 15.27578214 08
| Epoch (UTC): | 25 May 2026 13:55:55 |
| Eccentricity: | 0.0001094 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.1417° |
| argument of perigee: | 275.7094° |
| revolutions per day: | 15.27578214 |
| mean anomaly at epoch: | 84.3633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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