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 62481U 26145.50201520 +.00000000 +00000-0 +10422-2 0 00008
2 62481 43.0022 302.2976 0001742 260.4838 99.5816 15.27593210 01
| Epoch (UTC): | 25 May 2026 12:02:54 |
| Eccentricity: | 0.0001742 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.2976° |
| argument of perigee: | 260.4838° |
| revolutions per day: | 15.27593210 |
| mean anomaly at epoch: | 99.5816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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