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 03814U 26088.13473433 +.00000000 +00000-0 +73303-3 0 00000
2 03814 62.2662 149.4002 0767985 11.7697 350.0156 12.79343977 07
| Epoch (UTC): | 29 March 2026 03:14:01 |
| Eccentricity: | 0.0767985 |
| inclination: | 62.2662° |
| perigee height: | 751 km |
| apogee height: | 1937 km |
| right ascension of ascending node: | 149.4002° |
| argument of perigee: | 11.7697° |
| revolutions per day: | 12.79343977 |
| mean anomaly at epoch: | 350.0156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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