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 60573U 26145.14339965 +.00000000 +00000-0 +10566-3 0 00003
2 60573 97.6780 219.6488 0004196 140.4330 219.7197 14.94878474 05
| Epoch (UTC): | 25 May 2026 03:26:29 |
| Eccentricity: | 0.0004196 |
| inclination: | 97.6780° |
| perigee height: | 580 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 219.6488° |
| argument of perigee: | 140.4330° |
| revolutions per day: | 14.94878474 |
| mean anomaly at epoch: | 219.7197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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