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 52842U 26145.11754003 +.00000000 +00000-0 +55199-4 0 00006
2 52842 53.2137 50.9463 0001633 83.9358 276.1820 15.08837598 00
| Epoch (UTC): | 25 May 2026 02:49:15 |
| Eccentricity: | 0.0001633 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 50.9463° |
| argument of perigee: | 83.9358° |
| revolutions per day: | 15.08837598 |
| mean anomaly at epoch: | 276.1820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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