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 49449U 26145.54280150 +.00000000 +00000-0 +83219-3 0 00002
2 49449 53.2158 201.3333 0002903 358.5790 1.5210 15.47408044 08
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0002903 |
| inclination: | 53.2158° |
| perigee height: | 422 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 201.3333° |
| argument of perigee: | 358.5790° |
| revolutions per day: | 15.47408044 |
| mean anomaly at epoch: | 1.5210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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