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 49207U 26145.07381149 +.00000000 +00000-0 +25263-4 0 00008
2 49207 87.9163 340.0594 0001713 104.5639 255.5683 13.18685722 00
| Epoch (UTC): | 25 May 2026 01:46:17 |
| Eccentricity: | 0.0001713 |
| inclination: | 87.9163° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0594° |
| argument of perigee: | 104.5639° |
| revolutions per day: | 13.18685722 |
| mean anomaly at epoch: | 255.5683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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