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 00059U 26069.94965684 +.00000000 +00000-0 +86183-4 0 00001
2 00059 28.2486 268.3105 0188976 211.0813 147.8431 13.53164577 06
| Epoch (UTC): | 10 March 2026 22:47:30 |
| Eccentricity: | 0.0188976 |
| inclination: | 28.2486° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 268.3105° |
| argument of perigee: | 211.0813° |
| revolutions per day: | 13.53164577 |
| mean anomaly at epoch: | 147.8431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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