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 63872U 26145.42466470 +.00000000 +00000-0 +28679-3 0 00005
2 63872 70.0022 41.1357 0002750 268.2434 91.8410 14.98326349 05
| Epoch (UTC): | 25 May 2026 10:11:31 |
| Eccentricity: | 0.0002750 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.1357° |
| argument of perigee: | 268.2434° |
| revolutions per day: | 14.98326349 |
| mean anomaly at epoch: | 91.8410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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