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 26129.85397216 +.00000000 +00000-0 +28417-4 0 00004
2 00059 28.2505 320.4960 0188910 353.9918 5.8375 13.53168175 05
| Epoch (UTC): | 09 May 2026 20:29:43 |
| Eccentricity: | 0.0188910 |
| inclination: | 28.2505° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 320.4960° |
| argument of perigee: | 353.9918° |
| revolutions per day: | 13.53168175 |
| mean anomaly at epoch: | 5.8375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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