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 58284U 26145.19475442 +.00000000 +00000-0 +47846-3 0 00006
2 58284 97.3869 236.8584 0005828 217.9724 142.1120 15.55601602 04
| Epoch (UTC): | 25 May 2026 04:40:26 |
| Eccentricity: | 0.0005828 |
| inclination: | 97.3869° |
| perigee height: | 396 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 236.8584° |
| argument of perigee: | 217.9724° |
| revolutions per day: | 15.55601602 |
| mean anomaly at epoch: | 142.1120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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