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 60498U 26145.46269951 +.00000000 +00000-0 +31504-3 0 00006
2 60498 97.3906 227.0774 0003808 19.8705 340.2684 15.30018126 05
| Epoch (UTC): | 25 May 2026 11:06:17 |
| Eccentricity: | 0.0003808 |
| inclination: | 97.3906° |
| perigee height: | 473 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 227.0774° |
| argument of perigee: | 19.8705° |
| revolutions per day: | 15.30018126 |
| mean anomaly at epoch: | 340.2684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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