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 49215U 26145.37958120 +.00000000 +00000-0 +31827-3 0 00001
2 49215 87.9177 278.9861 0001074 113.2295 246.8951 13.20773264 08
| Epoch (UTC): | 25 May 2026 09:06:35 |
| Eccentricity: | 0.0001074 |
| inclination: | 87.9177° |
| perigee height: | 1181 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9861° |
| argument of perigee: | 113.2295° |
| revolutions per day: | 13.20773264 |
| mean anomaly at epoch: | 246.8951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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