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 58364U 26145.42980875 +.00000000 +00000-0 +12158-2 0 00009
2 58364 43.0000 289.9999 0008547 300.5501 59.4500 15.08227490 09
| Epoch (UTC): | 25 May 2026 10:18:55 |
| Eccentricity: | 0.0008547 |
| inclination: | 43.0000° |
| perigee height: | 536 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 289.9999° |
| argument of perigee: | 300.5501° |
| revolutions per day: | 15.08227490 |
| mean anomaly at epoch: | 59.4500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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