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 49171U 26145.24996185 +.00000000 +00000-0 +10872-2 0 00007
2 49171 69.9912 90.6494 0004315 194.3011 165.8035 15.13577297 09
| Epoch (UTC): | 25 May 2026 05:59:56 |
| Eccentricity: | 0.0004315 |
| inclination: | 69.9912° |
| perigee height: | 522 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 90.6494° |
| argument of perigee: | 194.3011° |
| revolutions per day: | 15.13577297 |
| mean anomaly at epoch: | 165.8035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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