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 58108U 26145.32705966 +.00000000 +00000-0 +62901-4 0 00003
2 58108 53.1599 155.9680 0001187 85.8320 274.2818 15.34395153 04
| Epoch (UTC): | 25 May 2026 07:50:57 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.9680° |
| argument of perigee: | 85.8320° |
| revolutions per day: | 15.34395153 |
| mean anomaly at epoch: | 274.2818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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