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 26040.16731848 +.00000000 +00000-0 +41218-3 0 00005
2 00012 32.9003 316.4223 1646698 147.1743 224.2833 11.48527654 07
| Epoch (UTC): | 09 February 2026 04:00:56 |
| Eccentricity: | 0.1646698 |
| inclination: | 32.9003° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 316.4223° |
| argument of perigee: | 147.1743° |
| revolutions per day: | 11.48527654 |
| mean anomaly at epoch: | 224.2833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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