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 49212U 26145.23062178 +.00000000 +00000-0 +44404-4 0 00008
2 49212 87.9160 340.0279 0002478 93.0708 267.0708 13.18685807 01
| Epoch (UTC): | 25 May 2026 05:32:05 |
| Eccentricity: | 0.0002478 |
| inclination: | 87.9160° |
| perigee height: | 1188 km |
| apogee height: | 1192 km |
| right ascension of ascending node: | 340.0279° |
| argument of perigee: | 93.0708° |
| revolutions per day: | 13.18685807 |
| mean anomaly at epoch: | 267.0708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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