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 62769U 26145.49320500 +.00000000 +00000-0 +62423-3 0 00004
2 62769 53.1615 325.4611 0001218 94.9270 265.1870 15.30206379 03
| Epoch (UTC): | 25 May 2026 11:50:12 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 325.4611° |
| argument of perigee: | 94.9270° |
| revolutions per day: | 15.30206379 |
| mean anomaly at epoch: | 265.1870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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