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 52649U 26144.73803044 +.00000000 +00000-0 +29137-4 0 00001
2 52649 53.2147 277.5780 0001311 93.6623 266.4519 15.08836151 02
| Epoch (UTC): | 24 May 2026 17:42:45 |
| Eccentricity: | 0.0001311 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 277.5780° |
| argument of perigee: | 93.6623° |
| revolutions per day: | 15.08836151 |
| mean anomaly at epoch: | 266.4519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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