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 50848U 26145.42988706 +.00000000 +00000-0 -23793-4 0 00009
2 50848 53.2103 194.6222 0001422 84.9104 275.2050 15.08841024 06
| Epoch (UTC): | 25 May 2026 10:19:02 |
| Eccentricity: | 0.0001422 |
| inclination: | 53.2103° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.6222° |
| argument of perigee: | 84.9104° |
| revolutions per day: | 15.08841024 |
| mean anomaly at epoch: | 275.2050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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