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 62123U 26145.49993606 +.00000000 +00000-0 +59798-3 0 00002
2 62123 42.9999 62.6075 0001072 221.4716 138.6054 15.27608107 01
| Epoch (UTC): | 25 May 2026 11:59:54 |
| Eccentricity: | 0.0001072 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.6075° |
| argument of perigee: | 221.4716° |
| revolutions per day: | 15.27608107 |
| mean anomaly at epoch: | 138.6054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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