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 58822U 26145.49151580 +.00000000 +00000-0 +28903-3 0 00004
2 58822 97.4367 226.2325 0008574 277.2684 82.7579 15.24811016 02
| Epoch (UTC): | 25 May 2026 11:47:46 |
| Eccentricity: | 0.0008574 |
| inclination: | 97.4367° |
| perigee height: | 485 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 226.2325° |
| argument of perigee: | 277.2684° |
| revolutions per day: | 15.24811016 |
| mean anomaly at epoch: | 82.7579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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