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 26047.08016656 +.00000000 +00000-0 +59196-4 0 00002
2 00059 28.2499 25.8204 0188866 19.1088 341.6431 13.53161724 00
| Epoch (UTC): | 16 February 2026 01:55:26 |
| Eccentricity: | 0.0188866 |
| inclination: | 28.2499° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 25.8204° |
| argument of perigee: | 19.1088° |
| revolutions per day: | 13.53161724 |
| mean anomaly at epoch: | 341.6431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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