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 62455U 26145.35337044 +.00000000 +00000-0 +00000-0 0 00002
2 62455 0.0663 44.5498 0001516 15.5411 226.9666 1.00270786 01
| Epoch (UTC): | 25 May 2026 08:28:51 |
| Eccentricity: | 0.0001516 |
| inclination: | 0.0663° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 44.5498° |
| argument of perigee: | 15.5411° |
| revolutions per day: | 1.00270786 |
| mean anomaly at epoch: | 226.9666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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