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 26032.07456598 +.00000000 +00000-0 +25555-3 0 00009
2 03669 88.4549 159.2981 1707870 163.0417 203.5847 11.30395398 02
| Epoch (UTC): | 01 February 2026 01:47:22 |
| Eccentricity: | 0.1707870 |
| inclination: | 88.4549° |
| perigee height: | 576 km |
| apogee height: | 3441 km |
| right ascension of ascending node: | 159.2981° |
| argument of perigee: | 163.0417° |
| revolutions per day: | 11.30395398 |
| mean anomaly at epoch: | 203.5847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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