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 60602U 26145.16957140 +.00000000 +00000-0 +39939-4 0 00005
2 60602 53.1623 310.8715 0001013 99.0265 261.0852 15.34388015 09
| Epoch (UTC): | 25 May 2026 04:04:10 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.1623° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 310.8715° |
| argument of perigee: | 99.0265° |
| revolutions per day: | 15.34388015 |
| mean anomaly at epoch: | 261.0852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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