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 60904U 26145.63397534 +.00000000 +00000-0 +77621-5 0 00008
2 60904 53.1586 111.6439 0000792 99.2212 260.8895 15.69705808 04
| Epoch (UTC): | 25 May 2026 15:12:55 |
| Eccentricity: | 0.0000792 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 111.6439° |
| argument of perigee: | 99.2212° |
| revolutions per day: | 15.69705808 |
| mean anomaly at epoch: | 260.8895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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