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 58881U 26145.66668980 +.00000000 +00000-0 -11049-3 0 00009
2 58881 53.1601 324.7096 0001567 80.6480 109.0668 15.33565728 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001567 |
| inclination: | 53.1601° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 324.7096° |
| argument of perigee: | 80.6480° |
| revolutions per day: | 15.33565728 |
| mean anomaly at epoch: | 109.0668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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