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 52120U 26145.23669066 +.00000000 +00000-0 +39841-4 0 00008
2 52120 53.2128 95.4877 0001304 90.6219 269.4922 15.08836708 08
| Epoch (UTC): | 25 May 2026 05:40:50 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.4877° |
| argument of perigee: | 90.6219° |
| revolutions per day: | 15.08836708 |
| mean anomaly at epoch: | 269.4922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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