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 11060U 26138.03729308 +.00000000 +00000-0 +61359-4 0 00001
2 11060 98.4548 160.4542 0009764 336.6300 23.4432 14.19365567 02
| Epoch (UTC): | 18 May 2026 00:53:42 |
| Eccentricity: | 0.0009764 |
| inclination: | 98.4548° |
| perigee height: | 820 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 160.4542° |
| argument of perigee: | 336.6300° |
| revolutions per day: | 14.19365567 |
| mean anomaly at epoch: | 23.4432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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