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 26097.11331035 +.00000000 +00000-0 +10266-3 0 00003
2 12792 74.0289 231.2326 0012427 96.0428 264.2143 14.39023492 06
| Epoch (UTC): | 07 April 2026 02:43:10 |
| Eccentricity: | 0.0012427 |
| inclination: | 74.0289° |
| perigee height: | 753 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 231.2326° |
| argument of perigee: | 96.0428° |
| revolutions per day: | 14.39023492 |
| mean anomaly at epoch: | 264.2143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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