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 12472U 26053.20572323 +.00000000 +00000-0 +00000-0 0 00009
2 12472 9.5636 316.4083 0004851 334.9968 208.3032 1.00213665 04
| Epoch (UTC): | 22 February 2026 04:56:14 |
| Eccentricity: | 0.0004851 |
| inclination: | 9.5636° |
| perigee height: | 35782 km |
| apogee height: | 35823 km |
| right ascension of ascending node: | 316.4083° |
| argument of perigee: | 334.9968° |
| revolutions per day: | 1.00213665 |
| mean anomaly at epoch: | 208.3032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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