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 39451U 26031.92084876 +.00000000 +00000-0 +16296-3 0 00008
2 39451 87.7429 23.6339 0002799 98.4741 261.6825 15.27480344 05
| Epoch (UTC): | 31 January 2026 22:06:01 |
| Eccentricity: | 0.0002799 |
| inclination: | 87.7429° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 23.6339° |
| argument of perigee: | 98.4741° |
| revolutions per day: | 15.27480344 |
| mean anomaly at epoch: | 261.6825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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