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 49283U 26145.42351716 +.00000000 +00000-0 +47427-3 0 00003
2 49283 87.9175 278.9728 0002637 90.2075 269.9360 13.20771500 00
| Epoch (UTC): | 25 May 2026 10:09:51 |
| Eccentricity: | 0.0002637 |
| inclination: | 87.9175° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9728° |
| argument of perigee: | 90.2075° |
| revolutions per day: | 13.20771500 |
| mean anomaly at epoch: | 269.9360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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