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 12527U 26065.15039536 +.00000000 +00000-0 +59680-3 0 00002
2 12527 102.1445 36.1838 0037962 227.0299 202.2479 12.38097940 02
| Epoch (UTC): | 06 March 2026 03:36:34 |
| Eccentricity: | 0.0037962 |
| inclination: | 102.1445° |
| perigee height: | 1485 km |
| apogee height: | 1545 km |
| right ascension of ascending node: | 36.1838° |
| argument of perigee: | 227.0299° |
| revolutions per day: | 12.38097940 |
| mean anomaly at epoch: | 202.2479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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