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 26071.04330890 +.00000000 +00000-0 +69225-4 0 00005
2 12792 74.0275 279.3514 0013096 154.3554 205.8252 14.39010040 01
| Epoch (UTC): | 12 March 2026 01:02:21 |
| Eccentricity: | 0.0013096 |
| inclination: | 74.0275° |
| perigee height: | 752 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 279.3514° |
| argument of perigee: | 154.3554° |
| revolutions per day: | 14.39010040 |
| mean anomaly at epoch: | 205.8252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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