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 14452U 26040.28297493 +.00000000 +00000-0 +73293-4 0 00003
2 14452 81.1624 126.3146 0089511 213.5240 146.0257 14.27239976 09
| Epoch (UTC): | 09 February 2026 06:47:29 |
| Eccentricity: | 0.0089511 |
| inclination: | 81.1624° |
| perigee height: | 737 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 126.3146° |
| argument of perigee: | 213.5240° |
| revolutions per day: | 14.27239976 |
| mean anomaly at epoch: | 146.0257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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