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 02124U 26088.00049073 +.00000000 +00000-0 +75963-4 0 00003
2 02124 144.5103 14.3034 0081321 256.0328 103.1294 13.87831035 04
| Epoch (UTC): | 29 March 2026 00:00:42 |
| Eccentricity: | 0.0081321 |
| inclination: | 144.5103° |
| perigee height: | 877 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 14.3034° |
| argument of perigee: | 256.0328° |
| revolutions per day: | 13.87831035 |
| mean anomaly at epoch: | 103.1294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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