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 20169U 26045.21202044 +.00000000 +00000-0 -40363-3 0 00003
2 20169 7.3776 5.2997 7190432 251.6844 23.6745 2.26414260 02
| Epoch (UTC): | 14 February 2026 05:05:18 |
| Eccentricity: | 0.7190432 |
| inclination: | 7.3776° |
| perigee height: | 505 km |
| apogee height: | 35735 km |
| right ascension of ascending node: | 5.2997° |
| argument of perigee: | 251.6844° |
| revolutions per day: | 2.26414260 |
| mean anomaly at epoch: | 23.6745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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