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 26154.17880031 +.00000000 +00000-0 +11716-3 0 00008
2 28523 82.9503 56.1694 0038309 20.5076 339.7615 13.88074785 08
| Epoch (UTC): | 03 June 2026 04:17:28 |
| Eccentricity: | 0.0038309 |
| inclination: | 82.9503° |
| perigee height: | 907 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 56.1694° |
| argument of perigee: | 20.5076° |
| revolutions per day: | 13.88074785 |
| mean anomaly at epoch: | 339.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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