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 65091U 26145.04681789 +.00000000 +00000-0 +67129-3 0 00003
2 65091 53.1585 29.6315 0000969 71.1628 288.9483 15.42163851 03
| Epoch (UTC): | 25 May 2026 01:07:25 |
| Eccentricity: | 0.0000969 |
| inclination: | 53.1585° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 29.6315° |
| argument of perigee: | 71.1628° |
| revolutions per day: | 15.42163851 |
| mean anomaly at epoch: | 288.9483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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