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 26044.77401536 +.00000000 +00000-0 +35368-3 0 00003
2 00012 32.9006 300.1845 1646772 171.5778 191.6410 11.48533378 00
| Epoch (UTC): | 13 February 2026 18:34:34 |
| Eccentricity: | 0.1646772 |
| inclination: | 32.9006° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 300.1845° |
| argument of perigee: | 171.5778° |
| revolutions per day: | 11.48533378 |
| mean anomaly at epoch: | 191.6410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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