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 26137.78201953 +.00000000 +00000-0 +72652-4 0 00004
2 12792 74.0274 156.1803 0013330 5.1993 354.9297 14.39039632 07
| Epoch (UTC): | 17 May 2026 18:46:06 |
| Eccentricity: | 0.0013330 |
| inclination: | 74.0274° |
| perigee height: | 752 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 156.1803° |
| argument of perigee: | 5.1993° |
| revolutions per day: | 14.39039632 |
| mean anomaly at epoch: | 354.9297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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