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 49157U 26145.50946947 +.00000000 +00000-0 +33677-3 0 00000
2 49157 69.9979 76.0561 0003558 196.5836 163.5211 15.05352689 04
| Epoch (UTC): | 25 May 2026 12:13:38 |
| Eccentricity: | 0.0003558 |
| inclination: | 69.9979° |
| perigee height: | 548 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 76.0561° |
| argument of perigee: | 196.5836° |
| revolutions per day: | 15.05352689 |
| mean anomaly at epoch: | 163.5211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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