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 28523U 26039.20480604 +.00000000 +00000-0 +99052-4 0 00006
2 28523 82.9522 143.1637 0037015 348.4494 11.5816 13.88052617 00
| Epoch (UTC): | 08 February 2026 04:54:55 |
| Eccentricity: | 0.0037015 |
| inclination: | 82.9522° |
| perigee height: | 908 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 143.1637° |
| argument of perigee: | 348.4494° |
| revolutions per day: | 13.88052617 |
| mean anomaly at epoch: | 11.5816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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