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 25175U 26150.47720269 +.00000000 +00000-0 +00000-0 0 00004
2 25175 30.0771 211.3731 5294765 39.5095 349.1398 4.38911543 02
| Epoch (UTC): | 30 May 2026 11:27:10 |
| Eccentricity: | 0.5294765 |
| inclination: | 30.0771° |
| perigee height: | 1036 km |
| apogee height: | 17722 km |
| right ascension of ascending node: | 211.3731° |
| argument of perigee: | 39.5095° |
| revolutions per day: | 4.38911543 |
| mean anomaly at epoch: | 349.1398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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