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 62184U 26144.90631993 +.00000000 +00000-0 -10381-3 0 00008
2 62184 70.0019 322.1946 0002270 266.2851 93.8048 14.98339716 01
| Epoch (UTC): | 24 May 2026 21:45:06 |
| Eccentricity: | 0.0002270 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 322.1946° |
| argument of perigee: | 266.2851° |
| revolutions per day: | 14.98339716 |
| mean anomaly at epoch: | 93.8048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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