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 63928U 26145.23735481 +.00000000 +00000-0 +28143-3 0 00003
2 63928 70.0007 81.6456 0002860 266.6102 93.4730 14.98340065 09
| Epoch (UTC): | 25 May 2026 05:41:47 |
| Eccentricity: | 0.0002860 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6456° |
| argument of perigee: | 266.6102° |
| revolutions per day: | 14.98340065 |
| mean anomaly at epoch: | 93.4730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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