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 26129.89547649 +.00000000 +00000-0 +72504-4 0 00000
2 00012 32.9145 0.1612 1647165 262.4181 78.7070 11.48607822 01
| Epoch (UTC): | 09 May 2026 21:29:29 |
| Eccentricity: | 0.1647165 |
| inclination: | 32.9145° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 0.1612° |
| argument of perigee: | 262.4181° |
| revolutions per day: | 11.48607822 |
| mean anomaly at epoch: | 78.7070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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