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 38038U 26088.21244244 +.00000000 +00000-0 +12085-3 0 00001
2 38038 98.4137 157.1748 0006473 176.3621 277.1149 14.38143283 03
| Epoch (UTC): | 29 March 2026 05:05:55 |
| Eccentricity: | 0.0006473 |
| inclination: | 98.4137° |
| perigee height: | 760 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 157.1748° |
| argument of perigee: | 176.3621° |
| revolutions per day: | 14.38143283 |
| mean anomaly at epoch: | 277.1149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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