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 60408U 26145.48587019 +.00000000 +00000-0 -69884-5 0 00002
2 60408 53.1585 67.7526 0001160 86.8013 273.3137 15.69715346 07
| Epoch (UTC): | 25 May 2026 11:39:39 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.1585° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 67.7526° |
| argument of perigee: | 86.8013° |
| revolutions per day: | 15.69715346 |
| mean anomaly at epoch: | 273.3137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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