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 60490U 26145.19532220 +.00000000 +00000-0 +37091-3 0 00007
2 60490 97.3778 227.5023 0003061 27.6658 332.4748 15.37012724 00
| Epoch (UTC): | 25 May 2026 04:41:15 |
| Eccentricity: | 0.0003061 |
| inclination: | 97.3778° |
| perigee height: | 453 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 227.5023° |
| argument of perigee: | 27.6658° |
| revolutions per day: | 15.37012724 |
| mean anomaly at epoch: | 332.4748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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