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 52639U 26145.63597150 +.00000000 +00000-0 +16793-4 0 00002
2 52639 53.2163 273.6937 0001170 84.8408 275.2718 15.08845625 01
| Epoch (UTC): | 25 May 2026 15:15:47 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.2163° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 273.6937° |
| argument of perigee: | 84.8408° |
| revolutions per day: | 15.08845625 |
| mean anomaly at epoch: | 275.2718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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