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 49210U 26145.19040705 +.00000000 +00000-0 -11171-3 0 00008
2 49210 87.8931 324.8247 0002441 96.1112 264.0296 13.13461502 00
| Epoch (UTC): | 25 May 2026 04:34:11 |
| Eccentricity: | 0.0002441 |
| inclination: | 87.8931° |
| perigee height: | 1208 km |
| apogee height: | 1212 km |
| right ascension of ascending node: | 324.8247° |
| argument of perigee: | 96.1112° |
| revolutions per day: | 13.13461502 |
| mean anomaly at epoch: | 264.0296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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