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 58135U 26145.16313435 +.00000000 +00000-0 +87961-4 0 00004
2 58135 43.0057 60.5227 0001970 266.0884 93.9743 15.27573680 05
| Epoch (UTC): | 25 May 2026 03:54:54 |
| Eccentricity: | 0.0001970 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 60.5227° |
| argument of perigee: | 266.0884° |
| revolutions per day: | 15.27573680 |
| mean anomaly at epoch: | 93.9743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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