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 39161U 26032.40860851 +.00000000 +00000-0 +23632-3 0 00007
2 39161 97.7501 91.2778 0009730 98.2210 262.0107 14.80911789 02
| Epoch (UTC): | 01 February 2026 09:48:23 |
| Eccentricity: | 0.0009730 |
| inclination: | 97.7501° |
| perigee height: | 620 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 91.2778° |
| argument of perigee: | 98.2210° |
| revolutions per day: | 14.80911789 |
| mean anomaly at epoch: | 262.0107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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