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 62445U 26145.55811146 +.00000000 +00000-0 +70581-3 0 00007
2 62445 53.1601 338.5153 0001755 99.9852 260.1347 15.30204129 07
| Epoch (UTC): | 25 May 2026 13:23:40 |
| Eccentricity: | 0.0001755 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.5153° |
| argument of perigee: | 99.9852° |
| revolutions per day: | 15.30204129 |
| mean anomaly at epoch: | 260.1347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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