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 14373U 26088.16841638 +.00000000 +00000-0 +59267-4 0 00005
2 14373 82.5371 124.2788 0020832 74.9350 285.4170 14.86251905 09
| Epoch (UTC): | 29 March 2026 04:02:31 |
| Eccentricity: | 0.0020832 |
| inclination: | 82.5371° |
| perigee height: | 595 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 124.2788° |
| argument of perigee: | 74.9350° |
| revolutions per day: | 14.86251905 |
| mean anomaly at epoch: | 285.4170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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