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 14699U 26047.24482588 +.00000000 +00000-0 +25828-3 0 00000
2 14699 82.5466 129.1596 0014183 4.3014 355.8342 15.23527822 01
| Epoch (UTC): | 16 February 2026 05:52:32 |
| Eccentricity: | 0.0014183 |
| inclination: | 82.5466° |
| perigee height: | 485 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 129.1596° |
| argument of perigee: | 4.3014° |
| revolutions per day: | 15.23527822 |
| mean anomaly at epoch: | 355.8342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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