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 49458U 26145.50349078 +.00000000 +00000-0 +15749-3 0 00006
2 49458 53.2137 234.2900 0001004 86.8395 273.2712 15.08829783 02
| Epoch (UTC): | 25 May 2026 12:05:01 |
| Eccentricity: | 0.0001004 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 234.2900° |
| argument of perigee: | 86.8395° |
| revolutions per day: | 15.08829783 |
| mean anomaly at epoch: | 273.2712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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