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 60409U 26145.09404403 +.00000000 +00000-0 +13718-4 0 00008
2 60409 53.1591 69.5700 0000859 69.7336 290.3774 15.69716057 07
| Epoch (UTC): | 25 May 2026 02:15:25 |
| Eccentricity: | 0.0000859 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 69.5700° |
| argument of perigee: | 69.7336° |
| revolutions per day: | 15.69716057 |
| mean anomaly at epoch: | 290.3774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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