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 62480U 26145.42120877 +.00000000 +00000-0 +62931-3 0 00006
2 62480 42.9976 302.5529 0000638 264.6670 95.4109 15.27602373 07
| Epoch (UTC): | 25 May 2026 10:06:32 |
| Eccentricity: | 0.0000638 |
| inclination: | 42.9976° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 302.5529° |
| argument of perigee: | 264.6670° |
| revolutions per day: | 15.27602373 |
| mean anomaly at epoch: | 95.4109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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