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 26074.87852185 +.00000000 +00000-0 +46681-3 0 00008
2 39444 97.8184 44.5223 0037920 158.4050 201.8787 15.08026217 02
| Epoch (UTC): | 15 March 2026 21:05:04 |
| Eccentricity: | 0.0037920 |
| inclination: | 97.8184° |
| perigee height: | 516 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 44.5223° |
| argument of perigee: | 158.4050° |
| revolutions per day: | 15.08026217 |
| mean anomaly at epoch: | 201.8787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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