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 39091U 26063.45016345 +.00000000 +00000-0 +13733-3 0 00000
2 39091 98.3950 245.4888 0010050 186.6674 173.4381 14.36492679 09
| Epoch (UTC): | 04 March 2026 10:48:14 |
| Eccentricity: | 0.0010050 |
| inclination: | 98.3950° |
| perigee height: | 763 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 245.4888° |
| argument of perigee: | 186.6674° |
| revolutions per day: | 14.36492679 |
| mean anomaly at epoch: | 173.4381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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