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 62502U 26145.46033808 +.00000000 +00000-0 +43793-3 0 00007
2 62502 43.0002 215.3261 0001265 265.1802 94.8905 15.27590282 00
| Epoch (UTC): | 25 May 2026 11:02:53 |
| Eccentricity: | 0.0001265 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.3261° |
| argument of perigee: | 265.1802° |
| revolutions per day: | 15.27590282 |
| mean anomaly at epoch: | 94.8905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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