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 38332U 26145.60987948 +.00000000 +00000-0 +00000-0 0 00001
2 38332 0.0322 46.3950 0002492 29.3207 158.8863 1.00271914 09
| Epoch (UTC): | 25 May 2026 14:38:13 |
| Eccentricity: | 0.0002492 |
| inclination: | 0.0322° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 46.3950° |
| argument of perigee: | 29.3207° |
| revolutions per day: | 1.00271914 |
| mean anomaly at epoch: | 158.8863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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