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 26075.58820544 +.00000000 +00000-0 +47012-4 0 00004
2 14453 81.1653 131.5597 0103990 178.7934 181.3518 14.25441201 06
| Epoch (UTC): | 16 March 2026 14:07:00 |
| Eccentricity: | 0.0103990 |
| inclination: | 81.1653° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 131.5597° |
| argument of perigee: | 178.7934° |
| revolutions per day: | 14.25441201 |
| mean anomaly at epoch: | 181.3518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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