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 00503U 26152.17459147 +.00000000 +00000-0 +00000-0 0 00005
2 00503 47.5063 85.7508 2836361 199.0509 325.4183 7.78166541 01
| Epoch (UTC): | 01 June 2026 04:11:24 |
| Eccentricity: | 0.2836361 |
| inclination: | 47.5063° |
| perigee height: | 1328 km |
| apogee height: | 7430 km |
| right ascension of ascending node: | 85.7508° |
| argument of perigee: | 199.0509° |
| revolutions per day: | 7.78166541 |
| mean anomaly at epoch: | 325.4183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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