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 39439U 26056.58007542 +.00000000 +00000-0 +21832-2 0 00009
2 39439 97.7294 54.1216 0008783 172.3292 187.8135 16.26924483 07
| Epoch (UTC): | 25 February 2026 13:55:18 |
| Eccentricity: | 0.0008783 |
| inclination: | 97.7294° |
| perigee height: | 195 km |
| apogee height: | 207 km |
| right ascension of ascending node: | 54.1216° |
| argument of perigee: | 172.3292° |
| revolutions per day: | 16.26924483 |
| mean anomaly at epoch: | 187.8135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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