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 62178U 26145.20676308 +.00000000 +00000-0 +38209-3 0 00002
2 62178 70.0016 321.6358 0002879 264.0776 96.0055 14.98336432 04
| Epoch (UTC): | 25 May 2026 04:57:44 |
| Eccentricity: | 0.0002879 |
| inclination: | 70.0016° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 321.6358° |
| argument of perigee: | 264.0776° |
| revolutions per day: | 14.98336432 |
| mean anomaly at epoch: | 96.0055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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