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 26073.80295413 +.00000000 +00000-0 +12780-3 0 00005
2 00029 48.3774 113.1612 0022660 223.5861 136.3263 14.78640417 00
| Epoch (UTC): | 14 March 2026 19:16:15 |
| Eccentricity: | 0.0022660 |
| inclination: | 48.3774° |
| perigee height: | 618 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 113.1612° |
| argument of perigee: | 223.5861° |
| revolutions per day: | 14.78640417 |
| mean anomaly at epoch: | 136.3263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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