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 62177U 26145.45946829 +.00000000 +00000-0 +38207-3 0 00004
2 62177 70.0018 330.9173 0003003 268.6380 91.4436 14.98339803 01
| Epoch (UTC): | 25 May 2026 11:01:38 |
| Eccentricity: | 0.0003003 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.9173° |
| argument of perigee: | 268.6380° |
| revolutions per day: | 14.98339803 |
| mean anomaly at epoch: | 91.4436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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