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 28368U 26150.42441175 +.00000000 +00000-0 +24299-3 0 00001
2 28368 98.1263 129.9715 0001611 116.0703 244.0676 14.83697052 03
| Epoch (UTC): | 30 May 2026 10:11:09 |
| Eccentricity: | 0.0001611 |
| inclination: | 98.1263° |
| perigee height: | 617 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 129.9715° |
| argument of perigee: | 116.0703° |
| revolutions per day: | 14.83697052 |
| mean anomaly at epoch: | 244.0676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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