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 49427U 26145.57712904 +.00000000 +00000-0 -10856-4 0 00007
2 49427 53.2131 243.9680 0001173 71.4996 288.6123 15.08837574 01
| Epoch (UTC): | 25 May 2026 13:51:03 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 243.9680° |
| argument of perigee: | 71.4996° |
| revolutions per day: | 15.08837574 |
| mean anomaly at epoch: | 288.6123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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