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 60472U 26145.10683861 +.00000000 +00000-0 +15283-3 0 00005
2 60472 97.3758 221.7910 0002438 43.6613 316.4817 15.23332022 05
| Epoch (UTC): | 25 May 2026 02:33:50 |
| Eccentricity: | 0.0002438 |
| inclination: | 97.3758° |
| perigee height: | 494 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 221.7910° |
| argument of perigee: | 43.6613° |
| revolutions per day: | 15.23332022 |
| mean anomaly at epoch: | 316.4817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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