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 59322U 26145.14520198 +.00000000 +00000-0 +68916-3 0 00005
2 59322 42.9884 96.8205 0023768 170.4172 189.7151 15.65505599 08
| Epoch (UTC): | 25 May 2026 03:29:05 |
| Eccentricity: | 0.0023768 |
| inclination: | 42.9884° |
| perigee height: | 356 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 96.8205° |
| argument of perigee: | 170.4172° |
| revolutions per day: | 15.65505599 |
| mean anomaly at epoch: | 189.7151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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