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 49187U 26145.46499757 +.00000000 +00000-0 +70915-4 0 00007
2 49187 87.9164 339.9792 0001994 90.4909 269.6452 13.18685446 02
| Epoch (UTC): | 25 May 2026 11:09:35 |
| Eccentricity: | 0.0001994 |
| inclination: | 87.9164° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9792° |
| argument of perigee: | 90.4909° |
| revolutions per day: | 13.18685446 |
| mean anomaly at epoch: | 269.6452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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