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 52134U 26145.24496270 +.00000000 +00000-0 -14718-3 0 00005
2 52134 53.2137 85.4510 0001552 77.4604 282.6562 15.08851008 09
| Epoch (UTC): | 25 May 2026 05:52:44 |
| Eccentricity: | 0.0001552 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 85.4510° |
| argument of perigee: | 77.4604° |
| revolutions per day: | 15.08851008 |
| mean anomaly at epoch: | 282.6562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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