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 12150U 26070.43138477 +.00000000 +00000-0 +13232-3 0 00008
2 12150 65.8192 79.7293 0042099 76.7843 283.7912 13.77469181 07
| Epoch (UTC): | 11 March 2026 10:21:11 |
| Eccentricity: | 0.0042099 |
| inclination: | 65.8192° |
| perigee height: | 942 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 79.7293° |
| argument of perigee: | 76.7843° |
| revolutions per day: | 13.77469181 |
| mean anomaly at epoch: | 283.7912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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