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 62091U 26145.13058470 +.00000000 +00000-0 +14136-2 0 00004
2 62091 43.0012 302.4644 0001376 300.5161 59.5571 15.70896481 07
| Epoch (UTC): | 25 May 2026 03:08:02 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0012° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 302.4644° |
| argument of perigee: | 300.5161° |
| revolutions per day: | 15.70896481 |
| mean anomaly at epoch: | 59.5571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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