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 49197U 26145.44430766 +.00000000 +00000-0 -65624-3 0 00002
2 49197 87.8949 324.7383 0001763 96.2634 263.8696 13.13468494 07
| Epoch (UTC): | 25 May 2026 10:39:48 |
| Eccentricity: | 0.0001763 |
| inclination: | 87.8949° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7383° |
| argument of perigee: | 96.2634° |
| revolutions per day: | 13.13468494 |
| mean anomaly at epoch: | 263.8696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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