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 26073.61555913 +.00000000 +00000-0 +71022-4 0 00003
2 12792 74.0272 274.6035 0013014 148.6821 211.5111 14.39011155 03
| Epoch (UTC): | 14 March 2026 14:46:24 |
| Eccentricity: | 0.0013014 |
| inclination: | 74.0272° |
| perigee height: | 752 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 274.6035° |
| argument of perigee: | 148.6821° |
| revolutions per day: | 14.39011155 |
| mean anomaly at epoch: | 211.5111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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