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 52705U 26145.31810756 +.00000000 +00000-0 -12472-3 0 00001
2 52705 53.2124 150.1211 0001331 59.0536 301.0587 15.08850971 03
| Epoch (UTC): | 25 May 2026 07:38:04 |
| Eccentricity: | 0.0001331 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 150.1211° |
| argument of perigee: | 59.0536° |
| revolutions per day: | 15.08850971 |
| mean anomaly at epoch: | 301.0587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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