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 60504U 26145.19132308 +.00000000 +00000-0 +23125-3 0 00009
2 60504 97.3784 225.5404 0003990 41.2307 318.9236 15.31450024 02
| Epoch (UTC): | 25 May 2026 04:35:30 |
| Eccentricity: | 0.0003990 |
| inclination: | 97.3784° |
| perigee height: | 469 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 225.5404° |
| argument of perigee: | 41.2307° |
| revolutions per day: | 15.31450024 |
| mean anomaly at epoch: | 318.9236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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