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 26047.98985000 +.00000000 +00000-0 +39595-3 0 00008
2 00012 32.9014 288.8492 1646852 188.6136 168.2463 11.48538048 02
| Epoch (UTC): | 16 February 2026 23:45:23 |
| Eccentricity: | 0.1646852 |
| inclination: | 32.9014° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 288.8492° |
| argument of perigee: | 188.6136° |
| revolutions per day: | 11.48538048 |
| mean anomaly at epoch: | 168.2463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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