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 62203U 26145.59979428 +.00000000 +00000-0 +51239-3 0 00000
2 62203 43.0003 196.3791 0001447 244.2602 115.8100 15.27613113 03
| Epoch (UTC): | 25 May 2026 14:23:42 |
| Eccentricity: | 0.0001447 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.3791° |
| argument of perigee: | 244.2602° |
| revolutions per day: | 15.27613113 |
| mean anomaly at epoch: | 115.8100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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