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 62079U 26145.40144477 +.00000000 +00000-0 +14197-4 0 00002
2 62079 97.4393 153.0567 0001571 86.6868 273.4546 15.19719339 03
| Epoch (UTC): | 25 May 2026 09:38:04 |
| Eccentricity: | 0.0001571 |
| inclination: | 97.4393° |
| perigee height: | 506 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 153.0567° |
| argument of perigee: | 86.6868° |
| revolutions per day: | 15.19719339 |
| mean anomaly at epoch: | 273.4546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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