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 53018U 26145.66668980 +.00000000 +00000-0 +10707-1 0 00003
2 53018 53.2267 92.6300 0001241 87.4030 91.6083 15.38873306 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.2267° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 92.6300° |
| argument of perigee: | 87.4030° |
| revolutions per day: | 15.38873306 |
| mean anomaly at epoch: | 91.6083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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