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 49052U 26145.39292253 +.00000000 +00000-0 +33452-3 0 00006
2 49052 37.0242 40.7887 0002937 358.9001 1.1738 15.08879642 01
| Epoch (UTC): | 25 May 2026 09:25:48 |
| Eccentricity: | 0.0002937 |
| inclination: | 37.0242° |
| perigee height: | 538 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 40.7887° |
| argument of perigee: | 358.9001° |
| revolutions per day: | 15.08879642 |
| mean anomaly at epoch: | 1.1738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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