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 60264U 26145.47298013 +.00000000 +00000-0 +22738-3 0 00008
2 60264 53.1607 55.8407 0001307 98.5289 261.5860 15.30153594 07
| Epoch (UTC): | 25 May 2026 11:21:05 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.8407° |
| argument of perigee: | 98.5289° |
| revolutions per day: | 15.30153594 |
| mean anomaly at epoch: | 261.5860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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