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 26020.18718419 +.00000000 +00000-0 +14497-2 0 00006
2 28188 49.4524 211.2339 4947933 88.2890 325.4643 5.74340916 08
| Epoch (UTC): | 20 January 2026 04:29:32 |
| Eccentricity: | 0.4947933 |
| inclination: | 49.4524° |
| perigee height: | 276 km |
| apogee height: | 13310 km |
| right ascension of ascending node: | 211.2339° |
| argument of perigee: | 88.2890° |
| revolutions per day: | 5.74340916 |
| mean anomaly at epoch: | 325.4643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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