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 27433U 26073.09479431 +.00000000 +00000-0 +25140-3 0 00002
2 27433 98.9322 121.8860 0014830 55.3760 304.8809 14.14623230 00
| Epoch (UTC): | 14 March 2026 02:16:30 |
| Eccentricity: | 0.0014830 |
| inclination: | 98.9322° |
| perigee height: | 833 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 121.8860° |
| argument of perigee: | 55.3760° |
| revolutions per day: | 14.14623230 |
| mean anomaly at epoch: | 304.8809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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