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 12967U 26150.59821610 +.00000000 +00000-0 +00000-0 0 00004
2 12967 12.1103 332.0304 0004125 336.5236 15.3123 1.00105262 02
| Epoch (UTC): | 30 May 2026 14:21:25 |
| Eccentricity: | 0.0004125 |
| inclination: | 12.1103° |
| perigee height: | 35816 km |
| apogee height: | 35851 km |
| right ascension of ascending node: | 332.0304° |
| argument of perigee: | 336.5236° |
| revolutions per day: | 1.00105262 |
| mean anomaly at epoch: | 15.3123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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