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 26137.80768073 +.00000000 +00000-0 -33667-5 0 00001
2 12150 65.8205 272.4898 0045359 37.4895 322.9317 13.77478413 01
| Epoch (UTC): | 17 May 2026 19:23:03 |
| Eccentricity: | 0.0045359 |
| inclination: | 65.8205° |
| perigee height: | 940 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 272.4898° |
| argument of perigee: | 37.4895° |
| revolutions per day: | 13.77478413 |
| mean anomaly at epoch: | 322.9317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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