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 26464U 26148.17842809 +.00000000 +00000-0 +00000-0 0 00005
2 26464 150.1226 48.2697 9032338 265.0681 3.6347 0.44417493 02
| Epoch (UTC): | 28 May 2026 04:16:56 |
| Eccentricity: | 0.9032338 |
| inclination: | 150.1226° |
| perigee height: | 643 km |
| apogee height: | 131721 km |
| right ascension of ascending node: | 48.2697° |
| argument of perigee: | 265.0681° |
| revolutions per day: | 0.44417493 |
| mean anomaly at epoch: | 3.6347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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