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 26070.60441838 +.00000000 +00000-0 +54835-4 0 00008
2 14453 81.1665 136.5798 0103726 193.2308 166.6148 14.25440042 08
| Epoch (UTC): | 11 March 2026 14:30:21 |
| Eccentricity: | 0.0103726 |
| inclination: | 81.1665° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 136.5798° |
| argument of perigee: | 193.2308° |
| revolutions per day: | 14.25440042 |
| mean anomaly at epoch: | 166.6148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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