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 03669U 26053.67334431 +.00000000 +00000-0 +11650-3 0 00000
2 03669 88.4555 156.9449 1707819 119.4583 258.7680 11.30408703 06
| Epoch (UTC): | 22 February 2026 16:09:36 |
| Eccentricity: | 0.1707819 |
| inclination: | 88.4555° |
| perigee height: | 576 km |
| apogee height: | 3441 km |
| right ascension of ascending node: | 156.9449° |
| argument of perigee: | 119.4583° |
| revolutions per day: | 11.30408703 |
| mean anomaly at epoch: | 258.7680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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