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 62441U 26145.52434258 +.00000000 +00000-0 +97841-3 0 00003
2 62441 53.1615 338.3098 0001748 90.6521 269.4680 15.30207551 01
| Epoch (UTC): | 25 May 2026 12:35:03 |
| Eccentricity: | 0.0001748 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.3098° |
| argument of perigee: | 90.6521° |
| revolutions per day: | 15.30207551 |
| mean anomaly at epoch: | 269.4680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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