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 36121U 26145.42090307 +.00000000 +00000-0 -13073-3 0 00007
2 36121 100.2212 31.1341 0021381 17.1823 343.0004 13.05082380 07
| Epoch (UTC): | 25 May 2026 10:06:06 |
| Eccentricity: | 0.0021381 |
| inclination: | 100.2212° |
| perigee height: | 1226 km |
| apogee height: | 1259 km |
| right ascension of ascending node: | 31.1341° |
| argument of perigee: | 17.1823° |
| revolutions per day: | 13.05082380 |
| mean anomaly at epoch: | 343.0004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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