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 58496U 26145.62092700 +.00000000 +00000-0 +16105-3 0 00005
2 58496 97.9260 228.6141 0010835 212.4364 147.6185 14.84190461 00
| Epoch (UTC): | 25 May 2026 14:54:08 |
| Eccentricity: | 0.0010835 |
| inclination: | 97.9260° |
| perigee height: | 609 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 228.6141° |
| argument of perigee: | 212.4364° |
| revolutions per day: | 14.84190461 |
| mean anomaly at epoch: | 147.6185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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