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 26049.14595100 +.00000000 +00000-0 +58244-4 0 00000
2 00059 28.2498 15.2061 0188880 36.4515 324.8730 13.53161946 07
| Epoch (UTC): | 18 February 2026 03:30:10 |
| Eccentricity: | 0.0188880 |
| inclination: | 28.2498° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 15.2061° |
| argument of perigee: | 36.4515° |
| revolutions per day: | 13.53161946 |
| mean anomaly at epoch: | 324.8730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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