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 60352U 26145.59846700 +.00000000 +00000-0 +58074-3 0 00003
2 60352 43.0164 53.4426 0016466 160.2318 199.9177 15.31639244 05
| Epoch (UTC): | 25 May 2026 14:21:47 |
| Eccentricity: | 0.0016466 |
| inclination: | 43.0164° |
| perigee height: | 460 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 53.4426° |
| argument of perigee: | 160.2318° |
| revolutions per day: | 15.31639244 |
| mean anomaly at epoch: | 199.9177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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