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 26046.12445434 +.00000000 +00000-0 +21096-3 0 00009
2 39161 97.7474 104.5330 0009419 59.9731 300.2415 14.80973919 09
| Epoch (UTC): | 15 February 2026 02:59:12 |
| Eccentricity: | 0.0009419 |
| inclination: | 97.7474° |
| perigee height: | 620 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 104.5330° |
| argument of perigee: | 59.9731° |
| revolutions per day: | 14.80973919 |
| mean anomaly at epoch: | 300.2415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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