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 26064.70810573 +.00000000 +00000-0 +85940-4 0 00009
2 14453 81.1674 142.5184 0103438 210.3854 149.1306 14.25438179 01
| Epoch (UTC): | 05 March 2026 16:59:40 |
| Eccentricity: | 0.0103438 |
| inclination: | 81.1674° |
| perigee height: | 733 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 142.5184° |
| argument of perigee: | 210.3854° |
| revolutions per day: | 14.25438179 |
| mean anomaly at epoch: | 149.1306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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