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 26145.62295953 +.00000000 +00000-0 +21342-3 0 00009
2 38038 98.4077 213.4023 0006908 26.1606 133.6571 14.38194330 00
| Epoch (UTC): | 25 May 2026 14:57:03 |
| Eccentricity: | 0.0006908 |
| inclination: | 98.4077° |
| perigee height: | 760 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 213.4023° |
| argument of perigee: | 26.1606° |
| revolutions per day: | 14.38194330 |
| mean anomaly at epoch: | 133.6571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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