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 55447U 26145.54836781 +.00000000 +00000-0 +94237-2 0 00005
2 55447 28.6508 335.3103 2271748 187.8005 168.0155 7.60560681 09
| Epoch (UTC): | 25 May 2026 13:09:38 |
| Eccentricity: | 0.2271748 |
| inclination: | 28.6508° |
| perigee height: | 2063 km |
| apogee height: | 7025 km |
| right ascension of ascending node: | 335.3103° |
| argument of perigee: | 187.8005° |
| revolutions per day: | 7.60560681 |
| mean anomaly at epoch: | 168.0155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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