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 00029U 26075.76262341 +.00000000 +00000-0 +99655-4 0 00003
2 00029 48.3774 103.8496 0022710 231.9125 127.9740 14.78642719 01
| Epoch (UTC): | 16 March 2026 18:18:10 |
| Eccentricity: | 0.0022710 |
| inclination: | 48.3774° |
| perigee height: | 618 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 103.8496° |
| argument of perigee: | 231.9125° |
| revolutions per day: | 14.78642719 |
| mean anomaly at epoch: | 127.9740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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