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 62603U 26145.22330604 +.00000000 +00000-0 +57571-3 0 00006
2 62603 43.0021 206.1868 0001370 262.8374 97.2322 15.27590831 09
| Epoch (UTC): | 25 May 2026 05:21:33 |
| Eccentricity: | 0.0001370 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 206.1868° |
| argument of perigee: | 262.8374° |
| revolutions per day: | 15.27590831 |
| mean anomaly at epoch: | 97.2322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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