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 26110.94634850 +.00000000 +00000-0 +11418-3 0 00003
2 00012 32.8988 66.9447 1646306 162.0641 204.5815 11.48597782 02
| Epoch (UTC): | 20 April 2026 22:42:44 |
| Eccentricity: | 0.1646306 |
| inclination: | 32.8988° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 66.9447° |
| argument of perigee: | 162.0641° |
| revolutions per day: | 11.48597782 |
| mean anomaly at epoch: | 204.5815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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