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 12032U 26148.29019965 +.00000000 +00000-0 +00000-0 0 00003
2 12032 70.1272 178.8289 5723518 240.2447 51.3274 2.00974203 05
| Epoch (UTC): | 28 May 2026 06:57:53 |
| Eccentricity: | 0.5723518 |
| inclination: | 70.1272° |
| perigee height: | 4965 km |
| apogee height: | 35327 km |
| right ascension of ascending node: | 178.8289° |
| argument of perigee: | 240.2447° |
| revolutions per day: | 2.00974203 |
| mean anomaly at epoch: | 51.3274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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