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 65173U 26145.59430939 +.00000000 +00000-0 +74991-4 0 00009
2 65173 86.4924 259.5908 0001924 95.7802 264.3552 13.24405662 02
| Epoch (UTC): | 25 May 2026 14:15:48 |
| Eccentricity: | 0.0001924 |
| inclination: | 86.4924° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.5908° |
| argument of perigee: | 95.7802° |
| revolutions per day: | 13.24405662 |
| mean anomaly at epoch: | 264.3552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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