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 26099.82457262 +.00000000 +00000-0 +84787-4 0 00004
2 12792 74.0294 226.2290 0012393 89.7633 270.4942 14.39025052 05
| Epoch (UTC): | 09 April 2026 19:47:23 |
| Eccentricity: | 0.0012393 |
| inclination: | 74.0294° |
| perigee height: | 753 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 226.2290° |
| argument of perigee: | 89.7633° |
| revolutions per day: | 14.39025052 |
| mean anomaly at epoch: | 270.4942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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