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 12792U 26070.76522753 +.00000000 +00000-0 +77536-4 0 00008
2 12792 74.0276 279.8647 0013135 154.8890 205.2906 14.39010124 09
| Epoch (UTC): | 11 March 2026 18:21:55 |
| Eccentricity: | 0.0013135 |
| inclination: | 74.0276° |
| perigee height: | 752 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 279.8647° |
| argument of perigee: | 154.8890° |
| revolutions per day: | 14.39010124 |
| mean anomaly at epoch: | 205.2906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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