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 60240U 26145.43134620 +.00000000 +00000-0 +20894-3 0 00002
2 60240 61.9953 304.9145 0047533 128.7761 231.7591 15.02640154 03
| Epoch (UTC): | 25 May 2026 10:21:08 |
| Eccentricity: | 0.0047533 |
| inclination: | 61.9953° |
| perigee height: | 526 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 304.9145° |
| argument of perigee: | 128.7761° |
| revolutions per day: | 15.02640154 |
| mean anomaly at epoch: | 231.7591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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