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 58054U 26145.46473788 +.00000000 +00000-0 +21851-2 0 00009
2 58054 43.0000 313.3076 0002946 290.9573 69.0963 15.27606069 05
| Epoch (UTC): | 25 May 2026 11:09:13 |
| Eccentricity: | 0.0002946 |
| inclination: | 43.0000° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 313.3076° |
| argument of perigee: | 290.9573° |
| revolutions per day: | 15.27606069 |
| mean anomaly at epoch: | 69.0963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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