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 43169U 26145.11421668 +.00000000 +00000-0 +14803-3 0 00002
2 43169 34.9964 302.1324 0002722 216.0173 144.0351 15.00884856 01
| Epoch (UTC): | 25 May 2026 02:44:28 |
| Eccentricity: | 0.0002722 |
| inclination: | 34.9964° |
| perigee height: | 562 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 302.1324° |
| argument of perigee: | 216.0173° |
| revolutions per day: | 15.00884856 |
| mean anomaly at epoch: | 144.0351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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