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 53719U 26145.55632413 +.00000000 +00000-0 +17203-3 0 00001
2 53719 53.2139 238.6741 0001298 78.8378 281.2760 15.08856159 06
| Epoch (UTC): | 25 May 2026 13:21:06 |
| Eccentricity: | 0.0001298 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 238.6741° |
| argument of perigee: | 78.8378° |
| revolutions per day: | 15.08856159 |
| mean anomaly at epoch: | 281.2760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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