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 28188U 26040.71775212 +.00000000 +00000-0 +10618-2 0 00002
2 28188 49.4483 192.7735 4942508 104.0376 313.8192 5.74818652 01
| Epoch (UTC): | 09 February 2026 17:13:33 |
| Eccentricity: | 0.4942508 |
| inclination: | 49.4483° |
| perigee height: | 279 km |
| apogee height: | 13292 km |
| right ascension of ascending node: | 192.7735° |
| argument of perigee: | 104.0376° |
| revolutions per day: | 5.74818652 |
| mean anomaly at epoch: | 313.8192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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