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 62459U 26145.55493612 +.00000000 +00000-0 +61758-3 0 00002
2 62459 54.9928 94.3336 0006415 98.4478 261.7290 15.65973301 06
| Epoch (UTC): | 25 May 2026 13:19:06 |
| Eccentricity: | 0.0006415 |
| inclination: | 54.9928° |
| perigee height: | 366 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 94.3336° |
| argument of perigee: | 98.4478° |
| revolutions per day: | 15.65973301 |
| mean anomaly at epoch: | 261.7290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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