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 63874U 26145.42047738 +.00000000 +00000-0 +16192-3 0 00006
2 63874 70.0025 41.1169 0002842 249.9736 110.1117 14.98334499 08
| Epoch (UTC): | 25 May 2026 10:05:29 |
| Eccentricity: | 0.0002842 |
| inclination: | 70.0025° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.1169° |
| argument of perigee: | 249.9736° |
| revolutions per day: | 14.98334499 |
| mean anomaly at epoch: | 110.1117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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