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 38667U 26098.72642413 +.00000000 +00000-0 +70336-4 0 00000
2 38667 74.0483 92.7233 0022062 281.2811 78.5863 14.36970112 00
| Epoch (UTC): | 08 April 2026 17:26:03 |
| Eccentricity: | 0.0022062 |
| inclination: | 74.0483° |
| perigee height: | 753 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 92.7233° |
| argument of perigee: | 281.2811° |
| revolutions per day: | 14.36970112 |
| mean anomaly at epoch: | 78.5863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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