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 14085U 26088.12826922 +.00000000 +00000-0 +10512-4 0 00000
2 14085 82.9431 228.9818 0034446 136.1286 224.2616 13.76592801 08
| Epoch (UTC): | 29 March 2026 03:04:42 |
| Eccentricity: | 0.0034446 |
| inclination: | 82.9431° |
| perigee height: | 951 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 228.9818° |
| argument of perigee: | 136.1286° |
| revolutions per day: | 13.76592801 |
| mean anomaly at epoch: | 224.2616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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