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 00012U 26088.16615596 +.00000000 +00000-0 +29381-3 0 00005
2 00012 32.8953 147.2493 1646093 41.3869 330.0385 11.48582051 02
| Epoch (UTC): | 29 March 2026 03:59:15 |
| Eccentricity: | 0.1646093 |
| inclination: | 32.8953° |
| perigee height: | 554 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 147.2493° |
| argument of perigee: | 41.3869° |
| revolutions per day: | 11.48582051 |
| mean anomaly at epoch: | 330.0385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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