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 67764U 26145.36180433 +.00000000 +00000-0 +56549-3 0 00001
2 67764 51.8844 208.7876 0005973 329.1169 30.9466 15.37865275 02
| Epoch (UTC): | 25 May 2026 08:40:59 |
| Eccentricity: | 0.0005973 |
| inclination: | 51.8844° |
| perigee height: | 448 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 208.7876° |
| argument of perigee: | 329.1169° |
| revolutions per day: | 15.37865275 |
| mean anomaly at epoch: | 30.9466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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