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 26044.94059066 +.00000000 +00000-0 +68826-4 0 00006
2 00059 28.2501 36.8139 0188888 1.1408 358.9545 13.53161584 05
| Epoch (UTC): | 13 February 2026 22:34:27 |
| Eccentricity: | 0.0188888 |
| inclination: | 28.2501° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 36.8139° |
| argument of perigee: | 1.1408° |
| revolutions per day: | 13.53161584 |
| mean anomaly at epoch: | 358.9545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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