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 12536U 26101.28620990 +.00000000 +00000-0 +28803-1 0 00008
2 12536 101.7537 202.1835 0482492 322.6766 56.0695 11.79542069 00
| Epoch (UTC): | 11 April 2026 06:52:08 |
| Eccentricity: | 0.0482492 |
| inclination: | 101.7537° |
| perigee height: | 1380 km |
| apogee height: | 2167 km |
| right ascension of ascending node: | 202.1835° |
| argument of perigee: | 322.6766° |
| revolutions per day: | 11.79542069 |
| mean anomaly at epoch: | 56.0695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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