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 39445U 26088.18171661 +.00000000 +00000-0 +78834-3 0 00006
2 39445 97.7902 55.6052 0035343 120.9790 239.4918 15.07118634 02
| Epoch (UTC): | 29 March 2026 04:21:40 |
| Eccentricity: | 0.0035343 |
| inclination: | 97.7902° |
| perigee height: | 521 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 55.6052° |
| argument of perigee: | 120.9790° |
| revolutions per day: | 15.07118634 |
| mean anomaly at epoch: | 239.4918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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