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 52139U 26145.54581186 +.00000000 +00000-0 +54720-4 0 00001
2 52139 53.2128 94.0976 0001405 83.2028 276.9124 15.08830020 09
| Epoch (UTC): | 25 May 2026 13:05:58 |
| Eccentricity: | 0.0001405 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 94.0976° |
| argument of perigee: | 83.2028° |
| revolutions per day: | 15.08830020 |
| mean anomaly at epoch: | 276.9124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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