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 26140.77293411 +.00000000 +00000-0 +33123-4 0 00000
2 00059 28.2481 264.3897 0188891 85.6576 276.5527 13.53168439 09
| Epoch (UTC): | 20 May 2026 18:33:01 |
| Eccentricity: | 0.0188891 |
| inclination: | 28.2481° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 264.3897° |
| argument of perigee: | 85.6576° |
| revolutions per day: | 13.53168439 |
| mean anomaly at epoch: | 276.5527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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