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 63938U 26145.55027088 +.00000000 +00000-0 +22956-3 0 00002
2 63938 70.0044 80.7360 0002165 265.8044 94.2868 14.98347623 07
| Epoch (UTC): | 25 May 2026 13:12:23 |
| Eccentricity: | 0.0002165 |
| inclination: | 70.0044° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.7360° |
| argument of perigee: | 265.8044° |
| revolutions per day: | 14.98347623 |
| mean anomaly at epoch: | 94.2868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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