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 26128.19369615 +.00000000 +00000-0 +41754-4 0 00003
2 14452 81.1635 37.4435 0089330 319.4274 40.0269 14.27265505 09
| Epoch (UTC): | 08 May 2026 04:38:55 |
| Eccentricity: | 0.0089330 |
| inclination: | 81.1635° |
| perigee height: | 737 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 37.4435° |
| argument of perigee: | 319.4274° |
| revolutions per day: | 14.27265505 |
| mean anomaly at epoch: | 40.0269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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