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 26150.63379110 +.00000000 +00000-0 -12156-2 0 00008
2 36121 100.2200 36.0724 0021239 5.4403 354.6931 13.05079931 04
| Epoch (UTC): | 30 May 2026 15:12:39 |
| Eccentricity: | 0.0021239 |
| inclination: | 100.2200° |
| perigee height: | 1226 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 36.0724° |
| argument of perigee: | 5.4403° |
| revolutions per day: | 13.05079931 |
| mean anomaly at epoch: | 354.6931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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