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 14453U 26076.07956455 +.00000000 +00000-0 +47242-4 0 00005
2 14453 81.1652 131.0648 0104015 177.3700 182.8050 14.25441333 05
| Epoch (UTC): | 17 March 2026 01:54:34 |
| Eccentricity: | 0.0104015 |
| inclination: | 81.1652° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 131.0648° |
| argument of perigee: | 177.3700° |
| revolutions per day: | 14.25441333 |
| mean anomaly at epoch: | 182.8050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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