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 38666U 26098.68460339 +.00000000 +00000-0 +66050-4 0 00007
2 38666 74.0449 93.8555 0028400 243.3054 116.5192 14.37812588 01
| Epoch (UTC): | 08 April 2026 16:25:49 |
| Eccentricity: | 0.0028400 |
| inclination: | 74.0449° |
| perigee height: | 745 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 93.8555° |
| argument of perigee: | 243.3054° |
| revolutions per day: | 14.37812588 |
| mean anomaly at epoch: | 116.5192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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