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 38756U 26155.23605375 +.00000000 +00000-0 +17186-3 0 00008
2 38756 98.2371 76.6253 0012145 93.8043 266.4558 14.82470490 05
| Epoch (UTC): | 04 June 2026 05:39:55 |
| Eccentricity: | 0.0012145 |
| inclination: | 98.2371° |
| perigee height: | 613 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 76.6253° |
| argument of perigee: | 93.8043° |
| revolutions per day: | 14.82470490 |
| mean anomaly at epoch: | 266.4558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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