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 49453U 26145.51917549 +.00000000 +00000-0 +88453-5 0 00000
2 49453 53.2171 234.3073 0001017 84.0771 276.0337 15.08834749 01
| Epoch (UTC): | 25 May 2026 12:27:36 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.2171° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 234.3073° |
| argument of perigee: | 84.0771° |
| revolutions per day: | 15.08834749 |
| mean anomaly at epoch: | 276.0337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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