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 26072.39169505 +.00000000 +00000-0 +14955-3 0 00004
2 12150 65.8192 74.8631 0042149 75.5733 285.0003 13.77469787 08
| Epoch (UTC): | 13 March 2026 09:24:02 |
| Eccentricity: | 0.0042149 |
| inclination: | 65.8192° |
| perigee height: | 942 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 74.8631° |
| argument of perigee: | 75.5733° |
| revolutions per day: | 13.77469787 |
| mean anomaly at epoch: | 285.0003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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