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 26067.44567955 +.00000000 +00000-0 +75947-4 0 00002
2 14453 81.1670 139.7613 0103560 202.3945 157.2698 14.25439159 03
| Epoch (UTC): | 08 March 2026 10:41:46 |
| Eccentricity: | 0.0103560 |
| inclination: | 81.1670° |
| perigee height: | 733 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 139.7613° |
| argument of perigee: | 202.3945° |
| revolutions per day: | 14.25439159 |
| mean anomaly at epoch: | 157.2698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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