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 52118U 26145.24406280 +.00000000 +00000-0 -21430-3 0 00008
2 52118 53.2143 95.4520 0001580 73.5279 286.5886 15.08822663 03
| Epoch (UTC): | 25 May 2026 05:51:27 |
| Eccentricity: | 0.0001580 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.4520° |
| argument of perigee: | 73.5279° |
| revolutions per day: | 15.08822663 |
| mean anomaly at epoch: | 286.5886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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