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 62736U 26145.16171181 +.00000000 +00000-0 +62023-3 0 00007
2 62736 42.9986 82.4350 0001845 255.1548 104.9099 15.27592596 07
| Epoch (UTC): | 25 May 2026 03:52:51 |
| Eccentricity: | 0.0001845 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 82.4350° |
| argument of perigee: | 255.1548° |
| revolutions per day: | 15.27592596 |
| mean anomaly at epoch: | 104.9099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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