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 62809U 26145.19663624 +.00000000 +00000-0 +73236-3 0 00007
2 62809 53.1603 314.1088 0001388 101.9862 258.1295 15.30221007 00
| Epoch (UTC): | 25 May 2026 04:43:09 |
| Eccentricity: | 0.0001388 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.1088° |
| argument of perigee: | 101.9862° |
| revolutions per day: | 15.30221007 |
| mean anomaly at epoch: | 258.1295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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