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 26042.28291959 +.00000000 +00000-0 +10752-2 0 00006
2 28188 49.4483 191.3656 4942134 105.2386 312.7860 5.74849714 00
| Epoch (UTC): | 11 February 2026 06:47:24 |
| Eccentricity: | 0.4942134 |
| inclination: | 49.4483° |
| perigee height: | 280 km |
| apogee height: | 13291 km |
| right ascension of ascending node: | 191.3656° |
| argument of perigee: | 105.2386° |
| revolutions per day: | 5.74849714 |
| mean anomaly at epoch: | 312.7860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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