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 26050.46728920 +.00000000 +00000-0 +23788-3 0 00002
2 28368 98.1165 28.3165 0002052 104.7090 255.4351 14.83330145 01
| Epoch (UTC): | 19 February 2026 11:12:53 |
| Eccentricity: | 0.0002052 |
| inclination: | 98.1165° |
| perigee height: | 617 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 28.3165° |
| argument of perigee: | 104.7090° |
| revolutions per day: | 14.83330145 |
| mean anomaly at epoch: | 255.4351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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