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 58376U 26145.30023748 +.00000000 +00000-0 +72819-4 0 00008
2 58376 53.1592 4.3203 0000955 76.9968 283.1141 15.34397914 08
| Epoch (UTC): | 25 May 2026 07:12:20 |
| Eccentricity: | 0.0000955 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 4.3203° |
| argument of perigee: | 76.9968° |
| revolutions per day: | 15.34397914 |
| mean anomaly at epoch: | 283.1141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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