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 62460U 26145.55484966 +.00000000 +00000-0 +62017-3 0 00005
2 62460 54.9932 94.3338 0006469 98.4014 261.7760 15.65989599 08
| Epoch (UTC): | 25 May 2026 13:18:59 |
| Eccentricity: | 0.0006469 |
| inclination: | 54.9932° |
| perigee height: | 366 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 94.3338° |
| argument of perigee: | 98.4014° |
| revolutions per day: | 15.65989599 |
| mean anomaly at epoch: | 261.7760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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