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 38046U 26081.01541948 +.00000000 +00000-0 +28269-3 0 00003
2 38046 97.1345 157.1435 0011085 256.3350 103.6719 16.45573094 08
| Epoch (UTC): | 22 March 2026 00:22:12 |
| Eccentricity: | 0.0011085 |
| inclination: | 97.1345° |
| perigee height: | 144 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 157.1435° |
| argument of perigee: | 256.3350° |
| revolutions per day: | 16.45573094 |
| mean anomaly at epoch: | 103.6719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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