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 39444U 26073.88321279 +.00000000 +00000-0 +64012-3 0 00001
2 39444 97.8183 43.5100 0037855 161.5965 198.6642 15.08011515 09
| Epoch (UTC): | 14 March 2026 21:11:49 |
| Eccentricity: | 0.0037855 |
| inclination: | 97.8183° |
| perigee height: | 516 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 43.5100° |
| argument of perigee: | 161.5965° |
| revolutions per day: | 15.08011515 |
| mean anomaly at epoch: | 198.6642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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