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 52114U 26145.25876466 +.00000000 +00000-0 +26850-4 0 00003
2 52114 53.2142 95.3860 0001198 95.0353 265.0776 15.08842500 03
| Epoch (UTC): | 25 May 2026 06:12:37 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.3860° |
| argument of perigee: | 95.0353° |
| revolutions per day: | 15.08842500 |
| mean anomaly at epoch: | 265.0776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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